KPL/PCK
 

P_constants (PcK) SPICE kernel file
===========================================================================

        By: Nat Bachman (NAIF)    2010 March 3
 
 
Purpose
--------------------------------------------------------

     This file makes available for use in SPICE-based application
     software orientation and size/shape data for natural bodies. The
     principal source of the data is a published report by the IAU/IAG
     Working Group on Cartographic Coordinates and Rotational Elements [1].

     Orientation and size/shape data not provided by this file may be
     available in mission-specific PCK files. Such PCKs may be the preferred
     data source for mission-related applications. Mission-specific PCKs can
     be found in PDS archives or on the NAIF web site at URL:

        http://naif.jpl.nasa.gov


File Organization
--------------------------------------------------------
 
     The contents of this file are as follows.
 
     Introductory Information:

         --   Purpose

         --   File Organization
 
         --   Version description
 
         --   Disclaimer
 
         --   Sources
 
         --   Explanatory notes
 
         --   Body numbers and names
 

     PcK Data:
 

        Orientation Data
        ----------------

         --   Orientation constants for the Sun and planets.        
              Additional items included in this section:

                 - Earth north geomagnetic centered dipole values
                   for epochs 1945-2000

                 - Mars prime meridian offset "lambda_a"

         --   Orientation constants for satellites
 
         --   Orientation constants for asteroids Eros, Gaspra, Ida,
              Itokawa, and Vesta
 
         --   Orientation constants for comets 19P/Borrelly
              and 9P/Tempel 1


        Radii of Bodies
        ---------------

         --   Radii of Sun and planets
         
         --   Radii of satellites, where available
         
         --   Radii of asteroids Ceres, Eros, Gaspra, Ida, Itokawa,
              Mathilde, Toutatis, and Vesta.
            
         --   Radii of comets 19P/Borrelly, Halley, 9P/Tempel 1,
              and 81P/Wild 2



Version Description
--------------------------------------------------------
 
     This file was created on March 3, 2010. This version
     incorporates data from reference [1].
 
     This file contains size, shape, and orientation data for all
     objects described by the previous version of the file, except
     for Kleopatra: a shape model for this body is not provided in [1]
     because, according to this source, it had been "modeled from
     low resolution radar data, and cannot be mapped from those
     data."

     New objects covered by this file but not the previous
     version are:
        
        19P/Borrelly
        Halley
        9P/Tempel 1
        81P/Wild 2
        Ceres
        Itokawa
        Mathilde
        Toutatis
                         
 
Disclaimer
--------------------------------------------------------
 
Applicability of Data

     This P_constants file may not contain the parameter values that
     you prefer. NAIF suggests that you inspect this file visually
     before proceeding with any critical or extended data processing.

File Modifications by Users

     Note that this file may be readily modified by you to change
     values or add/delete parameters. NAIF requests that you update the
     "by line," date, and version description section if you modify
     this file.
     
Known Limitations and Caveats

     Accuracy
     --------

     In general, the orientation models given here are claimed by the
     IAU/IAG Working Group Report [1] to be accurate to 0.1 degree
     ([1], p.158). However, NAIF notes that orientation models for
     natural satellites and asteroids have in some cases changed
     substantially with the availability of new observational data, so
     users are urged to investigate the suitability for their
     applications of the models presented here.

     Earth orientation
     -----------------

     NAIF strongly cautions against using the earth rotation model
     (from [1]) for work demanding high accuracy. This model has been
     determined by NAIF to have an error in the prime meridian location
     of magnitude at least 150 arcseconds, with a local minimum
     occurring during the year 1999. Regarding availability of better
     earth orientation data for use with the SPICE system:

        Earth orientation data are available from NAIF in the form of
        binary earth PCK files. NAIF employs an automated process to
        create these files; each time JPL's Tracking Systems and
        Applications Section produces a new earth orientation parameter
        (EOP) file, a new PCK is produced. These PCKs cover a roughly
        10 year time span starting at Jan. 1, 2000. In these PCK files,
        the following effects are accounted for in modeling the earth's
        rotation:

           - Precession:                   1976 IAU model

           - Nutation:                     1980 IAU model, plus interpolated
                                           EOP nutation corrections

           - Polar motion:                 interpolated from EOP file

           - True sidereal time:

                  UT1 - UT1R (if needed):  given by analytic formula
                + TAI - UT1 (or UT1R):     interpolated from EOP file
                + UT1 - GMST:              given by analytic formula
                + equation of equinoxes:   given by analytic formula

             where

                TAI    =   International Atomic Time
                UT1    =   Greenwich hour angle of computed mean sun - 12h
                UT1R   =   Regularized UT1
                GMST   =   Greenwich mean sidereal time                   

        These kernels are available from the NAIF web site

           http://naif.jpl.nasa.gov

        (follow the links to Data, generic_kernels, and PCK data) or

           ftp://naif.jpl.nasa.gov/pub/naif/generic_kernels/pck

        or via anonymous ftp from the server
 
           naif.jpl.nasa.gov

        The kernels are in the path

           pub/naif/generic_kernels/pck

        At this time, these kernels have file names of the form

           earth_000101_yymmdd_yymmdd.bpc

        The second and third dates are, respectively, the file's 
        coverage end time and the epoch of the last datum.
 
        These binary PCK files are very accurate (error < 0.1
        microradian) for epochs preceding the epoch of the last datum.
        For later epochs, the error rises to several microradians.

        Binary PCK files giving accurate earth orientation from 1972 to
        2007 and *low accuracy* predicted earth orientation from
        2007 to 2037 are also available in the same location. See the
        aareadme.txt file at the "pck" URL above for details.

        Characteristics and names of the binary kernels described here
        are subject to change. See the "pck" URL above for information
        on current binary earth PCKs.


     Lunar orientation
     -----------------

     The lunar orientation formula provided by this file is a
     trigonometric polynomial approximation yielding the orientation of
     the lunar "Mean Earth/Polar Axis" (ME) reference frame. A more
     accurate approximation can be obtained by using both the NAIF
     lunar frame kernel and the binary lunar orientation PCK file,
     which are available on the NAIF web site (see URLS above)
     and in the NAIF server's ftp area. The lunar frame kernel
     is located in the path

        pub/naif/generic_kernels/fk/satellites

     and has a name of the form

        moon_yymmdd.tf

     The binary lunar PCK is in the path

        pub/naif/generic_kernels/pck

     and has a name of the form

        moon_pa_dennn_yyyy-yyyy.bpc

     See the "aareadme.txt" files in the paths shown above for details
     on file contents and versions. We also suggest you refer to the
     SPICE tutorial named "lunar_earth_pck-fk," which is available from
     the NAIF web site.


     Earth geomagnetic dipole
     ------------------------

     The SPICE Toolkit doesn't currently contain software to model the
     earth's north geomagnetic centered dipole as a function of time.
     As a convenience for users, the north dipole location from the
     J2000 epoch was selected as a representative datum, and the
     planetocentric longitude and latitude of this location have been
     associated with the keywords
       
        BODY399_N_GEOMAG_CTR_DIPOLE_LON
        BODY399_N_GEOMAG_CTR_DIPOLE_LAT
     
     Values for the earth's north geomagnetic centered dipole are
     presented in comments as a discrete time series for the time range
     1945-2000. For details concerning the geomagnetic field model from
     which these values were derived, including a discussion of the
     model's accuracy, see [9].
 

     Mars prime meridian offset
     --------------------------

     The Mars prime meridian offset given by [5] is not used by
     SPICE geometry software for computations involving the shape
     of Mars (for example, in sub-observer point or surface intercept
     computations). The value is provided for informational
     purposes only.


     Software limitations
     --------------------

     SPICE Toolkits prior to version N0057 cannot make use of
     trigonometric polynomial terms in the formulas for orientation of
     the planets. The only planets for which such terms are used are
     Jupiter and Neptune. Use of trigonometric polynomial terms for
     natural satellites is and has been supported for all SPICE Toolkit
     versions.
 
     The second nutation precession angle (M2) for Mars is represented
     by a quadratic polynomial in the 2006 IAU report. The SPICELIB
     subroutine BODEUL can not handle this term (which is extremely
     small), so we truncate the polynomial to a linear one. The 
     resulting orientation error has a maximum magnitude of less
     than 0.0032 degrees over the time span 1996-2015 and less than
     0.0082 degrees over the time span 1986-2025.


Sources
--------------------------------------------------------
 
     The sources for the constants listed in this file are:


        [1]   Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F., 
              Conrad, A., Consolmagno, G.J., Hestroffer, D.,
              Hilton, J.L., Krasinsky, G.A., Neumann, G.,
              Oberst, J., Stooke, P., Tedesco, E.F., Tholen, D.J., 
              and Thomas, P.C. "Report of the IAU/IAG Working Group 
              on cartographic coordinates and rotational elements: 2006."

        [2]   Seidelmann, P.K., Archinal, B.A., A'Hearn, M.F., 
              Cruikshank, D.P., Hilton, J.L., Keller, H.U., Oberst, J.,
              Simon, J.L., Stooke, P., Tholen, D.J., and Thomas, P.C.
              "Report of the IAU/IAG Working Group on Cartographic
              Coordinates and Rotational Elements of the Planets and
              Satellites: 2003."
 
        [3]   Nautical Almanac Office, United States Naval Observatory
              and H.M. Nautical Almanac Office, Rutherford Appleton
              Laboratory (2010). "The Astronomical Almanac for
              the Year 2010," U.S. Government Printing Office,
              Washington, D.C.: and The Stationary Office, London.

        [4]   Nautical Almanac Office, United States Naval Observatory,
              H.M. Nautical Almanac Office, Royal Greenwich
              Observatory, Jet Propulsion Laboratory, Bureau des
              Longitudes, and The Time Service and Astronomy
              Departments, United States Naval Observatory (1992).
              "Explanatory Supplement to the Astronomical Almanac," P.
              Kenneth Seidelmann, ed. University Science Books, 20
              Edgehill Road, Mill Valley, CA 9494.

        [5]   Duxbury, Thomas C. (2001). "IAU/IAG 2000 Mars Cartographic
              Conventions,"  presentation to the Mars Express Data
              Archive Working Group, Dec. 14, 2001.

        [6]   Russell, C.T. and Luhmann, J.G. (1990). "Earth: Magnetic 
              Field and Magnetosphere." <http://www-ssc.igpp.ucla.
              edu/personnel/russell/papers/earth_mag>. Originally
              published in "Encyclopedia of Planetary Sciences," J.H.
              Shirley and R.W. Fainbridge, eds. Chapman and Hall,
              New York, pp 208-211.

        [7]   Russell, C.T. (1971). "Geophysical Coordinate 
              Transformations," Cosmic Electrodynamics 2  184-186.
              NAIF document 181.0.
     
        [8]   ESA/ESTEC Space Environment Information System (SPENVIS)
              (2003). Web page:  "Dipole approximations of the
              geomagnetic field."  <http://www.spenvis.oma.be/spenvis/
              help/background/magfield/cd.html>.
 
        [9]   International Association of Geomagnetism and Aeronomy
              and International Union of Geodesy and Geophysics (2004).
              Web page:  "The 9th Generation International Geomagnetic
              Reference Field." <http://www.ngdc.noaa.gov/
              IAGA/vmod/igrf.html>.
                             
        [10]  Davies, M.E., Abalakin, V.K., Bursa, M., Hunt, G.E.,
              and Lieske, J.H. (1989). "Report of the IAU/IAG/COSPAR
              Working Group on Cartographic Coordinates and Rotational
              Elements of the Planets and Satellites: 1988," Celestial
              Mechanics and Dynamical Astronomy, v.46, no.2, pp.
              187-204.

         
     Most values are from [1]. All exceptions are 
     commented where they occur in this file. The exceptions are:
 
                 
         --   Radii for the Sun are from [3].
             
         --   The second nutation precession angle (M2) for Mars is
              represented by a quadratic polynomial in the 2000
              IAU report. The SPICELIB subroutine BODEUL can not
              handle this term (which is extremely small), so we
              truncate the polynomial to a linear one.
           
          --  Earth north geomagnetic centered dipole values are from
              [8]. The article [6] was used to check most of 
              these values, and the values were also re-computed from 
              the 9th generation IGRF [9] by Nat Bachman.
         
          -- The Mars prime meridian offset angle is from [5].


     "Old values" listed are from the SPICE P_constants file
     pck00008.tpc dated September 21, 2004. Most of these values came
     from the 2003 IAU report [2].
 
 
 
 
Explanatory Notes
--------------------------------------------------------

     This file, which is logically part of the SPICE P-kernel, contains
     constants used to model the orientation, size and shape of the
     Sun, planets, natural satellites, and selected comets and
     asteroids. The orientation models express the direction of the
     pole and location of the prime meridian of a body as a function of
     time. The size/shape models ("shape models" for short) represent
     all bodies as ellipsoids, using two equatorial radii and a polar
     radius. Spheroids and spheres are obtained when two or all three
     radii are equal.

     The SPICE Toolkit routines that use this file are documented in
     the SPICE "Required Reading" file pck.req. They are also 
     documented in the "PCK" SPICE tutorial, which is available on
     the NAIF web site.

File Format
        
     A terse description of the PCK file format is given here. See the
     SPICE "Required Reading" files pck.req and kernel.req for a
     detailed explanation of the SPICE text kernel file format. The
     files pck.req and kernel.req are included in the documentation
     provided with the SPICE Toolkit.

     The file starts out with the ``ID word'' string

        KPL/PCK

     This string identifies the file as a text kernel containing PCK 
     data.

     This file consists of a series of comment blocks and data blocks.
     Comment blocks, which contain free-form descriptive or explanatory
     text, are preceded by a \begintext token. Data blocks follow a
     \begindata token. In order to be recognized, each of these tokens
     must be placed on a line by itself.

     The portion of the file preceding the first data block is treated
     as a comment block; it doesn't require an initial \begintext
     token.

     This file identifies data using a series of

        KEYWORD = VALUE

     assignments. The left hand side of each assignment is a
     "kernel variable" name; the right hand side is an associated value
     or list of values. The SPICE subroutine API allows SPICE routines
     and user applications to retrieve the set of values associated
     with each kernel variable name.

     Kernel variable names are case-sensitive and are limited to
     32 characters in length. 

     Numeric values may be integer or floating point. String values
     are normally limited to 80 characters in length; however, SPICE
     provides a mechanism for identifying longer, "continued" strings.
     See the SPICE routine STPOOL for details.

     String values are single quoted.

     When the right hand side of an assignment is a list of values,
     the list items may be separated by commas or simply by blanks.
     The list must be bracketed by parentheses. Example:

        BODY399_RADII = ( 6378.14 6378.14 6356.75 )
 
     Any blanks preceding or following keyword names, values and equal
     signs are ignored.
  
     Assignments may be spread over multiple lines, for example:

        BODY399_RADII = ( 6378.14 
                          6378.14 
                          6356.75 )

     This file may contain blank lines anywhere. Non-printing
     characters including TAB should not be present in the file: the
     presence of such characters may cause formatting errors when the
     file is viewed.

Time systems and reference frames

     The 2006 IAU/IAG Working Group Report [1] states the time scale
     used as the independent variable for the rotation formulas is
     Barycentric Dynamical Time (TDB) and that the epoch of variable
     quantities is J2000 TDB (2000 Jan 1 12:00 TDB). Throughout SPICE
     documentation and in this file, we use the names "J2000 TDB" and
     "J2000" for this epoch. The name "J2000.0" is equivalent.

     SPICE documentation refers to the time system used in this file 
     as either "ET" or "TDB." SPICE software makes no distinction 
     between TDB and the time system associated with the independent
     variable of the JPL planetary ephemerides T_eph.
 
     The inertial reference frame used for the rotational elements in
     this file is identified by [1] as the ICRF (International
     Celestial Reference Frame). 

     The SPICE PCK software that reads this file uses the label "J2000"
     to refer to the ICRF; this is actually a mislabeling which has
     been retained in the interest of backward compatibility. Using
     data from this file, by means of calls to the SPICE frame
     transformation routines, will actually compute orientation
     relative to the ICRF.

     The difference between the J2000 frame and the ICRF is
     on the order of tens of milliarcseconds and is well below the
     accuracy level of the formulas in this file.

Orientation models
 
     All of the orientation models use three Euler angles to describe
     the orientation of the coordinate axes of the "Body Equator and
     Prime Meridian" system with respect to an inertial system. By
     default, the inertial system is the ICRF (labeled as "J2000"), but
     other frames can be specified in the file. See the PCK Required
     Reading for details.
 
     The first two angles, in order, are the ICRF right ascension and
     declination (henceforth RA and DEC) of the north pole of a body as
     a function of time. The third angle is the prime meridian location
     (represented by "W"), which is expressed as a rotation about the
     north pole, and is also a function of time.
 
     For each body, the expressions for the north pole's right
     ascension and declination, as well as prime meridian location, are
     sums (as far as the models that appear in this file are concerned)
     of quadratic polynomials and trigonometric polynomials, where the
     independent variable is time.
 
     In this file, the time arguments in expressions always refer to
     Barycentric Dynamical Time (TDB), measured in centuries or days
     past a reference epoch. By default, the reference epoch is the
     J2000 epoch, which is Julian ephemeris date 2451545.0, but other
     epochs can be specified in the file. See the PCK Required Reading
     for details.

     Orientation models for satellites and some planets (including
     Jupiter) involve both polynomial terms and trigonometric terms.
     The arguments of the trigonometric terms are linear polynomials.
     In this file, we call the arguments of these trigonometric terms
     "nutation precession angles."

     Example: 2006 IAU Model for orientation of Jupiter.  Note that 
     these values are used as an example only; see the data area below 
     for current values.

        Right ascension
        ---------------
 
        alpha   =  268.056595 - 0.006499 T        +  0.000117 sin(Ja) 
             0                + 0.000938 sin(Jb)  +  0.001432 sin(Jc)
                              + 0.000030 sin(Jd)  +  0.002150 sin(Je)

        Declination
        -----------
 
        delta   =   64.495303 + 0.002413 T        +  0.000050 cos(Ja)
             0                + 0.000404 cos(Jb)  +  0.000617 cos(Jc)
                              - 0.000013 cos(Jd)  +  0.000926 cos(Je)

        Prime meridian
        --------------

        W       =  284.95  + 870.5366420 d
 

     Here

        T represents centuries past J2000 ( TDB ),
 
        d represents days past J2000 ( TDB ).

        Ja-Je are nutation precession angles.

     In this file, the polynomials' coefficients above are assigned 
     to kernel variable names (left-hand-side symbols) as follows

        BODY599_POLE_RA        = (   268.056595     -0.006499       0. )
        BODY599_POLE_DEC       = (    64.495303      0.002413       0. )
        BODY599_PM             = (   284.95        870.5366420      0. )

     and the trigonometric polynomials' coefficients are assigned 
     as follows

        BODY599_NUT_PREC_RA  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000117
                                                                0.000938
                                                                0.001432
                                                                0.000030
                                                                0.002150 )

        BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000050
                                                                0.000404
                                                                0.000617
                                                               -0.000013
                                                                0.000926 )

        BODY599_NUT_PREC_PM  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.0
                                                                0.0
                                                                0.0
                                                                0.0
                                                                0.0  ) 

     Note the number "599"; this is the NAIF ID code for Jupiter.

     In this file, the polynomial expressions for the nutation
     precession angles are listed along with the planet's RA, DEC, and
     prime meridian terms. Below are the 2006 IAU nutation precession
     angles for the Jupiter system.

        J1  =   73.32      +  91472.9 T
        J2  =   24.62      +  45137.2 T
        J3  =  283.90      +   4850.7 T
        J4  =  355.80      +   1191.3 T
        J5  =  119.90      +    262.1 T
        J6  =  229.80      +     64.3 T
        J7  =  352.25      +   2382.6 T
        J8  =  113.35      +   6070.0 T

        J9  =  146.64      + 182945.8 T
        J10 =   49.24      +  90274.4 T 

        Ja  =   99.360714  +   4850.4046 T
        Jb  =  175.895369  +   1191.9605 T
        Jc  =  300.323162  +    262.5475 T
        Jd  =  114.012305  +   6070.2476 T
        Je  =   49.511251  +     64.3000 T

     Here

        T represents centuries past J2000 ( TDB )

        J1-J10 and Ja-Je are the nutation precession angles. The angles
        J9 and J10 are equal to 2*J1 and 2*J2, respectively.
 
        Angles J9 and J10 are not present in [1]; they have been added
        to fit the terms 2*J1 and 2*J2, which appear in the orientation
        models of several satellites, into a form that can be accepted
        by the PCK system.

     The assignment of the nutation precession angles for the
     Jupiter system is as follows:
 
        BODY5_NUT_PREC_ANGLES  = (    73.32      91472.9
                                      24.62      45137.2
                                     283.90       4850.7
                                     355.80       1191.3
                                     119.90        262.1
                                     229.80         64.3
                                     352.25       2382.6
                                     113.35       6070.0   
                                     146.64     182945.8
                                      49.24      90274.4  
                                      99.360714   4850.4046
                                     175.895369   1191.9605
                                     300.323162    262.5475
                                     114.012305   6070.2476
                                      49.511251     64.3000  )

     You'll see an additional symbol grouped with the ones listed
     above; it is
 
        BODY599_LONG_AXIS
 
     This term is zero for all bodies except Mars. It represents the
     angular offset between the meridian containing the longest axis of
     the triaxial ellipsoid used to model a body's surface and the
     prime meridian of the body.

     The pattern of the formulas for satellite orientation is similar
     to that for Jupiter. Example: 2006 IAU values for Io. Again, these
     values are used as an example only; see the data area below for
     current values.
 
        Right ascension
        ---------------

        alpha  = 268.05  -  0.009 T  + 0.094 sin(J3)  +  0.024 sin(J4)
             0  

        Declination
        -----------

        delta  =  64.50  +  0.003 T  + 0.040 cos(J3)  +  0.011 cos(J4)
             0           
                          
        Prime meridian
        --------------

        W      = 200.39  +  203.4889538 d  -  0.085 sin(J3)  -  0.022 sin(J4)

 
        d represents days past J2000.
 
        J3 and J4 are nutation precession angles.
 
     The polynomial terms are assigned to symbols by the statements
 
        BODY501_POLE_RA       = (  268.05          -0.009      0. )
        BODY501_POLE_DEC      = (   64.50           0.003      0. )
        BODY501_PM            = (  200.39         203.4889538  0. )
 
     The coefficients of the trigonometric terms are assigned to symbols by
     the statements

        BODY501_NUT_PREC_RA   = (    0.   0.     0.094    0.024   )
        BODY501_NUT_PREC_DEC  = (    0.   0.     0.040    0.011   )
        BODY501_NUT_PREC_PM   = (    0.   0.    -0.085   -0.022   )

     501 is the NAIF ID code for Io.
 
     SPICE software expects the models for satellite orientation to
     follow the form of the model shown here: the polynomial portions of the
     RA, DEC, and W expressions are expected to be quadratic, the 
     trigonometric terms for RA and W (satellite prime meridian) are expected 
     to be linear combinations of sines of nutation precession angles, the 
     trigonometric terms for DEC are expected to be linear combinations of 
     cosines of nutation precession angles, and the polynomials for the 
     nutation precession angles themselves are expected to be linear.
 
     Eventually, the software will handle more complex expressions, we
     expect.
 
 
Shape models
 
     There is only one kind of shape model supported by the SPICE Toolkit
     software at present: the triaxial ellipsoid. The 2006 IAU report does
     not use any other models, except in the case of Mars, where 
     separate values are given for the north and south polar radii.
 
     For each body, three radii are listed:  The first number is
     the largest equatorial radius (the length of the semi-axis
     containing the prime meridian), the second number is the smaller
     equatorial radius, and the third is the polar radius.
 
     Example: Radii of the Earth.
 
        BODY399_RADII     = (     6378.14    6378.14      6356.75   )
 
 
Body Numbers and Names
--------------------------------------------------------
 
 
        1  Mercury barycenter
        2  Venus barycenter
        3  Earth barycenter
        4  Mars barycenter
        5  Jupiter barycenter
        6  Saturn barycenter
        7  Uranus barycenter
        8  Neptune barycenter
        9  Pluto barycenter
        10 Sun

 
        199 Mercury
 
 
        299 Venus
 
 
        399 Earth
 
        301 Moon
 
 
        499 Mars
 
        401 Phobos      402 Deimos
 
 
        599 Jupiter
 
        501 Io          502 Europa      503 Ganymede    504 Callisto
        505 Amalthea    506 Himalia     507 Elara       508 Pasiphae
        509 Sinope      510 Lysithea    511 Carme       512 Ananke
        513 Leda        514 Thebe       515 Adrastea    516 Metis
 
 
        699 Saturn
 
        601 Mimas       602 Enceladus   603 Tethys      604 Dione
        605 Rhea        606 Titan       607 Hyperion    608 Iapetus
        609 Phoebe      610 Janus       611 Epimetheus  612 Helene
        613 Telesto     614 Calypso     615 Atlas       616 Prometheus
        617 Pandora     618 Pan
 
 
        799 Uranus
 
        701 Ariel       702 Umbriel     703 Titania     704 Oberon
        705 Miranda     706 Cordelia    707 Ophelia     708 Bianca
        709 Cressida    710 Desdemona   711 Juliet      712 Portia
        713 Rosalind    714 Belinda     715 Puck
 
 
        899 Neptune
 
        801 Triton      802 Nereid      803 Naiad       804 Thalassa
        805 Despina     806 Galatea     807 Larissa     808 Proteus
 
 
        999 Pluto
 
        901 Charon
 
 
        1000005 Comet 19P/Borrelly
        1000036 Comet Halley
        1000093 Comet 9P/Tempel 1
        1000107 Comet 81P/Wild 2

        2000001 Asteroid Ceres
        2000004 Asteroid Vesta
        2000216 Asteroid Kleopatra
        2000253 Asteroid Mathilde
        2000433 Asteroid Eros
        2004179 Asteroid Toutatis
        2025143 Asteroid Itokawa
        2431010 Asteroid Ida
        9511010 Asteroid Gaspra
        
 
Orientation Constants for the Sun and Planets
--------------------------------------------------------
 
 
Sun
 
     Old values:

        Values are from the 2003 IAU report.

  
        body10_pole_ra         = (  286.13       0.          0. )
        body10_pole_dec        = (   63.87       0.          0. )
        body10_pm              = (   84.10      14.18440     0. )
        body10_long_axis       = (    0.                        )

     Current values:
 
        \begindata
 
        BODY10_POLE_RA         = (  286.13       0.          0. )
        BODY10_POLE_DEC        = (   63.87       0.          0. )
        BODY10_PM              = (   84.176     14.18440     0. )
        BODY10_LONG_AXIS       = (    0.                        )

        \begintext
 
Mercury
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.


     Current values:
  
        \begindata

        BODY199_POLE_RA          = (  281.01     -0.033      0. )
        BODY199_POLE_DEC         = (   61.45     -0.005      0. )
        BODY199_PM               = (  329.548     6.1385025  0. )
 
        BODY199_LONG_AXIS        = (    0.                        )
 
        \begintext
 
  
Venus
 
     Old values:
 
        Values are unchanged in the 2006 IAU report. 
 
     Current values:
 
        \begindata
 
        BODY299_POLE_RA          = (  272.76       0.          0. )
        BODY299_POLE_DEC         = (   67.16       0.          0. )
        BODY299_PM               = (  160.20      -1.4813688   0. )
 
        BODY299_LONG_AXIS        = (    0.                        )
 
        \begintext


Earth
 
     Old values:
 
        Values are unchanged in the 2006 report.
 
 
     Current values:
 
        \begindata 
 
        BODY399_POLE_RA        = (    0.      -0.641         0. )
        BODY399_POLE_DEC       = (   90.      -0.557         0. )
        BODY399_PM             = (  190.147  360.9856235     0. )
        BODY399_LONG_AXIS      = (    0.                        )

        \begintext


        Nutation precession angles for the Earth-Moon system:

           The linear coefficients have been scaled up from degrees/day
           to degrees/century, because the SPICELIB PCK reader expects
           these units.  The original constants were:
        
                                    125.045D0   -0.0529921D0
                                    250.089D0   -0.1059842D0
                                    260.008D0   13.0120009D0
                                    176.625D0   13.3407154D0
                                    357.529D0    0.9856003D0
                                    311.589D0   26.4057084D0
                                    134.963D0   13.0649930D0
                                    276.617D0    0.3287146D0
                                     34.226D0    1.7484877D0
                                     15.134D0   -0.1589763D0
                                    119.743D0    0.0036096D0
                                    239.961D0    0.1643573D0
                                     25.053D0   12.9590088D0 


        \begindata

       
        BODY3_NUT_PREC_ANGLES  = (  125.045         -1935.5364525000
                                    250.089         -3871.0729050000
                                    260.008        475263.3328725000  
                                    176.625        487269.6299850000
                                    357.529         35999.0509575000
                                    311.589        964468.4993100000
                                    134.963        477198.8693250000
                                    276.617         12006.3007650000
                                     34.226         63863.5132425000 
                                     15.134         -5806.6093575000
                                    119.743           131.8406400000
                                    239.961          6003.1503825000 
                                     25.053        473327.7964200000 )


        \begintext
 

     Earth north geomagnetic centered dipole:

        Old values:

           Values are from [7].  Note the year of publication was 1971.

           body399_mag_north_pole_lon  =  ( -69.761 )
           body399_mag_north_pole_lat  =  (  78.565 )


        Current values:

           The north dipole location is time-varying.  The values shown
           below, taken from [8], represent a discrete sampling of the
           north dipole location from 1945 to 2000. The terms DGRF and
           IGRF refer to, respectively, "Definitive Geomagnetic
           Reference Field" and "International Geomagnetic Reference
           Field."  See references [6], [8], and [9] for details.

           Coordinates are planetocentric. 

             Data source    Lat      Lon
             -----------   -----    ------
              DGRF 1945    78.47    291.47
              DGRF 1950    78.47    291.15
              DGRF 1955    78.46    290.84
              DGRF 1960    78.51    290.53
              DGRF 1965    78.53    290.15
              DGRF 1970    78.59    289.82
              DGRF 1975    78.69    289.53
              DGRF 1980    78.81    289.24 
              DGRF 1985    78.97    289.10
              DGRF 1990    79.13    288.89
              IGRF 1995    79.30    288.59
              IGRF 2000    79.54    288.43      


        Values are given for the epoch 2000 and are from the final row
        of the above table, which is from [8]. As shown by the table
        these values constitute a low-accuracy approximation for epochs
        not close to 2000.

        \begindata
       
        BODY399_N_GEOMAG_CTR_DIPOLE_LON  =  ( 288.43 )
        BODY399_N_GEOMAG_CTR_DIPOLE_LAT  =  (  79.54 )

        \begintext

 
Mars
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
   
     Current values:
 
        \begindata
 
        BODY499_POLE_RA          = (  317.68143   -0.1061      0.  )
        BODY499_POLE_DEC         = (   52.88650   -0.0609      0.  )
        BODY499_PM               = (  176.630    350.89198226  0.  )

        \begintext
 
        Source [5] specifies the following value for the lambda_a term
        (BODY499_LONG_AXIS ) for Mars. This term is the POSITIVE EAST
        LONGITUDE, measured from the prime meridian, of the meridian
        containing the longest axis of the reference ellipsoid.
        (CAUTION: previous values were POSITIVE WEST.)

           body499_long_axis        = (  252.  )
 
        We list this lambda_a value for completeness. The IAU report
        [1] gives equal values for both equatorial radii, so the
        lambda_a offset does not apply to the IAU model.
 
        The 2003 IAU report defines M2, the second nutation precession angle,
        by:
 
                                                2
           192.93  +  1128.4096700 d  +  8.864 T
 
        We truncate the M2 series to a linear expression, because the PCK
        software cannot handle the quadratic term.
 
        Again, the linear terms are scaled by 36525.0:
 
            -0.4357640000000000       -->     -15916.28010000000
          1128.409670000000           -->   41215163.19675000
            -1.8151000000000000E-02   -->       -662.9652750000000
 
        We also introduce a fourth nutation precession angle, which
        is the pi/2-complement of the third angle.  This angle is used
        in computing the prime meridian location for Deimos.  See the
        discussion of this angle below in the section containing orientation
        constants for Deimos.
 
        \begindata

        BODY4_NUT_PREC_ANGLES  = (  169.51     -15916.2801
                                    192.93   41215163.19675
                                     53.47       -662.965275
                                     36.53        662.965275  )
 
        \begintext
 
 
Jupiter
 
     Old values:
 
        Values are from the 2003 IAU report.


           body599_pole_ra        = (   268.05      -0.009       0. )
           body599_pole_dec       = (    64.49       0.003       0. )
           body599_pm             = (   284.95     870.5366420   0. )
           body599_long_axis      = (     0.                        )

           body5_nut_prec_angles  = (    73.32   91472.9
                                         24.62   45137.2
                                        283.90    4850.7
                                        355.80    1191.3
                                        119.90     262.1
                                        229.80      64.3
                                        352.35    2382.6
                                        113.35    6070.0   
                                        146.64  182945.8
                                         49.24   90274.4  )
 

                   
     Current values:
 
        The number of nutation precession angles is 15. The ninth and
        tenth are twice the first and second, respectively. The
        eleventh through fifteenth correspond to angles JA-JE in
        the 2006 IAU report; angles JA-JE were not used prior to that
        report.

        \begindata
 
 
        BODY599_POLE_RA        = (   268.056595     -0.006499       0. )
        BODY599_POLE_DEC       = (    64.495303      0.002413       0. )
        BODY599_PM             = (   284.95        870.5366420      0. )
        BODY599_LONG_AXIS      = (     0.                        )
 
        BODY599_NUT_PREC_RA  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000117
                                                                0.000938
                                                                0.001432
                                                                0.000030
                                                                0.002150 )

        BODY599_NUT_PREC_DEC = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.000050
                                                                0.000404
                                                                0.000617
                                                               -0.000013
                                                                0.000926 )

        BODY599_NUT_PREC_PM  = ( 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.  0.0
                                                                0.0
                                                                0.0
                                                                0.0
                                                                0.0  ) 


        BODY5_NUT_PREC_ANGLES  = (    73.32      91472.9
                                      24.62      45137.2
                                     283.90       4850.7
                                     355.80       1191.3
                                     119.90        262.1
                                     229.80         64.3
                                     352.25       2382.6
                                     113.35       6070.0   
                                     146.64     182945.8
                                      49.24      90274.4  
                                      99.360714   4850.4046
                                     175.895369   1191.9605
                                     300.323162    262.5475
                                     114.012305   6070.2476
                                      49.511251     64.3000  )
        \begintext
 
 
Saturn
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.

     Current values:
 
        \begindata

        BODY699_POLE_RA        = (    40.589    -0.036      0.  )
        BODY699_POLE_DEC       = (    83.537    -0.004      0.  )
        BODY699_PM             = (    38.90    810.7939024  0.  )
        BODY699_LONG_AXIS      = (     0.                       )
 
        \begintext
 
        The first seven angles given here are the angles S1 
        through S7 from the 2000 report; the eighth and
        ninth angles are 2*S1 and 2*S2, respectively.
 
 
        \begindata

        BODY6_NUT_PREC_ANGLES  = (  353.32   75706.7
                                     28.72   75706.7  
                                    177.40  -36505.5 
                                    300.00   -7225.9 
                                    316.45     506.2
                                    345.20   -1016.3  
                                     29.80     -52.1
                                    706.64  151413.4
                                     57.44  151413.4  )
        \begintext
 
 
Uranus
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
 
     Current values:
 
        \begindata
 
        BODY799_POLE_RA        = (  257.311     0.         0.  )
        BODY799_POLE_DEC       = (  -15.175     0.         0.  )
        BODY799_PM             = (  203.81   -501.1600928  0.  )
        BODY799_LONG_AXIS      = (    0.                       )
 
        \begintext
        
        The first 16 angles given here are the angles U1 
        through U16 from the 2000 report; the 17th and
        18th angles are 2*U11 and 2*U12, respectively.
        
        \begindata
         
        BODY7_NUT_PREC_ANGLES  = (  115.75   54991.87
                                    141.69   41887.66
                                    135.03   29927.35
                                     61.77   25733.59  
                                    249.32   24471.46
                                     43.86   22278.41 
                                     77.66   20289.42  
                                    157.36   16652.76  
                                    101.81   12872.63   
                                    138.64    8061.81
                                    102.23   -2024.22 
                                    316.41    2863.96  
                                    304.01     -51.94  
                                    308.71     -93.17 
                                    340.82     -75.32 
                                    259.14    -504.81 
                                    204.46   -4048.44
                                    632.82    5727.92     )
                                    
        \begintext
 
 
 
Neptune
 
     Old values:
 
        Values are unchanged in the 2006 IAU report. 
 
     Current values:

        \begindata        
 
           BODY899_POLE_RA        = (  299.36     0.         0. )
           BODY899_POLE_DEC       = (   43.46     0.         0. )
           BODY899_PM             = (  253.18   536.3128492  0. )
           BODY899_LONG_AXIS      = (    0.                     )


           BODY899_NUT_PREC_RA    = (  0.70 0. 0. 0. 0. 0. 0. 0. ) 
           BODY899_NUT_PREC_DEC   = ( -0.51 0. 0. 0. 0. 0. 0. 0. )
           BODY899_NUT_PREC_PM    = ( -0.48 0. 0. 0. 0. 0. 0. 0. )

        \begintext
 
           The 2000 report defines the nutation precession angles
 
              N, N1, N2, ... , N7
 
           and also uses the multiples of N1 and N7
 
              2*N1
 
           and
 
              2*N7, 3*N7, ..., 9*N7
 
           In this file, we treat the angles and their multiples as
           separate angles.  In the kernel variable
 
              BODY8_NUT_PREC_ANGLES
 
           the order of the angles is
 
              N, N1, N2, ... , N7, 2*N1, 2*N7, 3*N7, ..., 9*N7
 
           Each angle is defined by a linear polynomial, so two
           consecutive array elements are allocated for each
           angle.  The first term of each pair is the constant term,
           the second is the linear term.
 
        \begindata 

              BODY8_NUT_PREC_ANGLES = (   357.85         52.316
                                          323.92      62606.6
                                          220.51      55064.2 
                                          354.27      46564.5
                                           75.31      26109.4 
                                           35.36      14325.4
                                          142.61       2824.6  
                                          177.85         52.316 
                                          647.840    125213.200
                                          355.700       104.632
                                          533.550       156.948
                                          711.400       209.264
                                          889.250       261.580
                                         1067.100       313.896
                                         1244.950       366.212
                                         1422.800       418.528
                                         1600.650       470.844   )
                                         
        \begintext
 
 
 
Pluto
 
     Old values:
 
        Values are from the 2003 IAU report. 
 
        BODY999_POLE_RA        = (  313.02    0.         0.   )
        BODY999_POLE_DEC       = (    9.09    0.         0.   )
        BODY999_PM             = (  236.77  -56.3623195  0.   )
        BODY999_LONG_AXIS      = (    0.                      )


     Current values:
 
        \begindata
 
        BODY999_POLE_RA        = (  312.993   0.          0. )
        BODY999_POLE_DEC       = (    6.163   0.          0. )
        BODY999_PM             = (  237.305  -56.3625225  0. )
        BODY999_LONG_AXIS      = (    0.                     )

        \begintext
 
 
 
 
Orientation constants for the satellites
--------------------------------------------------------
 
 
Satellites of Earth
 
     Old values:
 
        Values are unchanged in the 2006 IAU report. 

 
     New values:
 
        \begindata
 
 



        BODY301_POLE_RA      = (  269.9949        0.0031        0.      )
        BODY301_POLE_DEC     = (   66.5392        0.0130        0.      )
        BODY301_PM           = (   38.3213       13.17635815   -1.4D-12 )
        BODY301_LONG_AXIS    = (    0.                                  )
   
        BODY301_NUT_PREC_RA  = (   -3.8787   -0.1204   0.0700   -0.0172
                                    0.0       0.0072   0.0       0.0
                                    0.0      -0.0052   0.0       0.0
                                    0.0043                              )
        
        BODY301_NUT_PREC_DEC = (   1.5419     0.0239  -0.0278    0.0068
                                   0.0       -0.0029   0.0009    0.0
                                   0.0        0.0008   0.0       0.0     
                                  -0.0009                               )
        
        BODY301_NUT_PREC_PM  = (   3.5610     0.1208  -0.0642    0.0158
                                   0.0252    -0.0066  -0.0047   -0.0046
                                   0.0028     0.0052   0.0040    0.0019
                                  -0.0044                               )
        \begintext
 

 
Satellites of Mars
 
 
     Phobos
 
          Old values:
 
             Values are unchanged in the 2006 IAU report.
 
          Current values:
 
            The quadratic prime meridian term is scaled by 1/36525**2:
 
               8.864000000000000   --->   6.6443009930565219E-09
 
        \begindata
 
          BODY401_POLE_RA  = ( 317.68    -0.108     0.                     )
          BODY401_POLE_DEC = (  52.90    -0.061     0.                     )
          BODY401_PM       = (  35.06  1128.8445850 6.6443009930565219E-09 )
                                       
          BODY401_LONG_AXIS     = (    0.   )
 
          BODY401_NUT_PREC_RA   = (   1.79    0.    0.   0. )
          BODY401_NUT_PREC_DEC  = (  -1.08    0.    0.   0. )
          BODY401_NUT_PREC_PM   = (  -1.42   -0.78  0.   0. )


        \begintext
 
 
     Deimos
 
        Old values:
 
           Values are unchanged in the 2006 IAU report.
 
 
        New values:
 
           The Deimos prime meridian expression is:
 
 
                                                     2
              W = 79.41  +  285.1618970 d  -  0.520 T  -  2.58 sin M
                                                                    3
 
                                                       +  0.19 cos M .
                                                                    3
 
 
           At the present time, the PCK kernel software (the routine
           BODEUL in particular) cannot handle the cosine term directly,
           but we can represent it as
 
              0.19 sin M
                        4
 
           where
 
              M   =  90.D0 - M
               4              3
 
           Therefore, the nutation precession angle assignments for Phobos
           and Deimos contain four coefficients rather than three.
 
           The quadratic prime meridian term is scaled by 1/36525**2:
 
              -0.5200000000000000  --->   -3.8978300049519307E-10
 
        \begindata
 
           BODY402_POLE_RA       = (  316.65     -0.108       0.           )
           BODY402_POLE_DEC      = (   53.52     -0.061       0.           )
           BODY402_PM            = (   79.41    285.1618970  -3.897830D-10 )
           BODY402_LONG_AXIS     = (    0.                                 )
 
           BODY402_NUT_PREC_RA   = (    0.   0.   2.98    0.   )
           BODY402_NUT_PREC_DEC  = (    0.   0.  -1.78    0.   )
           BODY402_NUT_PREC_PM   = (    0.   0.  -2.58    0.19 )

        \begintext
 
 
 
 
Satellites of Jupiter
 
 
     Io
 
          Old values:
 
             Values are unchanged in the 2006 IAU report.
 
          Current values:
         
        \begindata
 
        BODY501_POLE_RA       = (  268.05          -0.009      0. )
        BODY501_POLE_DEC      = (   64.50           0.003      0. )
        BODY501_PM            = (  200.39         203.4889538  0. )
        BODY501_LONG_AXIS     = (    0.                           )
 
        BODY501_NUT_PREC_RA   = (    0.   0.     0.094    0.024   )
        BODY501_NUT_PREC_DEC  = (    0.   0.     0.040    0.011   )
        BODY501_NUT_PREC_PM   = (    0.   0.    -0.085   -0.022   )

        \begintext
 
 
 
     Europa
 
 
        Old values:

           Values are from the 2003 IAU report.


        body502_pole_ra       = (  268.08          -0.009      0.   )
        body502_pole_dec      = (   64.51           0.003      0.   )
        body502_pm            = (   35.67         101.3747235  0.   )
        body502_long_axis     = (    0.                             )
 
        body502_nut_prec_ra   = ( 0. 0. 0.   1.086   0.060   0.015   0.009 )
        body502_nut_prec_dec  = ( 0. 0. 0.   0.468   0.026   0.007   0.002 )
        body502_nut_prec_pm   = ( 0. 0. 0.  -0.980  -0.054  -0.014  -0.008 )
        

        Current values:
 
        \begindata 
 
        BODY502_POLE_RA       = (  268.08          -0.009      0.   )
        BODY502_POLE_DEC      = (   64.51           0.003      0.   )
        BODY502_PM            = (   36.022        101.3747235  0.   )
        BODY502_LONG_AXIS     = (    0.                             )
 
        BODY502_NUT_PREC_RA   = ( 0. 0. 0.   1.086   0.060   0.015   0.009 )
        BODY502_NUT_PREC_DEC  = ( 0. 0. 0.   0.468   0.026   0.007   0.002 )
        BODY502_NUT_PREC_PM   = ( 0. 0. 0.  -0.980  -0.054  -0.014  -0.008 )
 
        \begintext
 
 
     Ganymede
 
        Old values:
 
             Values are unchanged in the 2006 IAU report.
 

        Current values:
        
        \begindata
    
        BODY503_POLE_RA       = (  268.20         -0.009       0.  )
        BODY503_POLE_DEC      = (   64.57          0.003       0.  )
        BODY503_PM            = (   44.064        50.3176081   0.  )
        BODY503_LONG_AXIS     = (    0.                            )

        BODY503_NUT_PREC_RA   = ( 0. 0. 0.  -0.037   0.431   0.091   )
        BODY503_NUT_PREC_DEC  = ( 0. 0. 0.  -0.016   0.186   0.039   )
        BODY503_NUT_PREC_PM   = ( 0. 0. 0.   0.033  -0.389  -0.082   )
 
        \begintext
 
 
     Callisto
 
        Old values:

             Values are unchanged in the 2006 IAU report.
        
        
        Current values:
        
        
        \begindata
  
        BODY504_POLE_RA       = (   268.72    -0.009       0.  )
        BODY504_POLE_DEC      = (    64.83     0.003       0.  )
        BODY504_PM            = (   259.51    21.5710715   0.  )
        BODY504_LONG_AXIS     = (     0.                       )
 
        BODY504_NUT_PREC_RA   = ( 0. 0. 0. 0.  -0.068   0.590  0.   0.010 )
        BODY504_NUT_PREC_DEC  = ( 0. 0. 0. 0.  -0.029   0.254  0.  -0.004 )
        BODY504_NUT_PREC_PM   = ( 0. 0. 0. 0.   0.061  -0.533  0.  -0.009 )
 
        \begintext
 
 
     Amalthea
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report.        
        
        Current values:
         
        \begindata
 
        BODY505_POLE_RA       = (   268.05    -0.009      0.  )
        BODY505_POLE_DEC      = (    64.49     0.003      0.  )
        BODY505_PM            = (   231.67   722.6314560  0.  )
        BODY505_LONG_AXIS     = (     0.                      )
 
        BODY505_NUT_PREC_RA  = ( -0.84  0. 0. 0. 0. 0. 0. 0.   0.01  0. )
        BODY505_NUT_PREC_DEC = ( -0.36  0. 0. 0. 0. 0. 0. 0.   0.    0. )
        BODY505_NUT_PREC_PM  = (  0.76  0. 0. 0. 0. 0. 0. 0.  -0.01  0. )
 
        \begintext
 
 
     Thebe
 
 
        Old values:
                
           Values are unchanged in the 2006 IAU report.                
          
        Current values:
        
        \begindata
 
        BODY514_POLE_RA       = (  268.05     -0.009       0.  )
        BODY514_POLE_DEC      = (   64.49      0.003       0.  )
        BODY514_PM            = (    8.56    533.7004100   0.  )
        BODY514_LONG_AXIS     = (    0.                        )
 
        BODY514_NUT_PREC_RA  = ( 0.  -2.11  0. 0. 0. 0. 0. 0. 0.  0.04 )
        BODY514_NUT_PREC_DEC = ( 0.  -0.91  0. 0. 0. 0. 0. 0. 0.  0.01 )
        BODY514_NUT_PREC_PM  = ( 0.   1.91  0. 0. 0. 0. 0. 0. 0. -0.04 )
 
        \begintext
 
 
     Adrastea
 
        Old values:
                
           Values are unchanged in the 2006 IAU report.                
        
        Current values:
        
        \begindata
 
 
 
        BODY515_POLE_RA       = (  268.05     -0.009       0.  )
        BODY515_POLE_DEC      = (   64.49      0.003       0.  )
        BODY515_PM            = (   33.29   1206.9986602   0.  )
        BODY515_LONG_AXIS     = (    0.                        )

        \begintext
 
 
     Metis
  
        Old values:
        
           Values are unchanged in the 2006 IAU report.  
              
        Current values:
           
        \begindata

        BODY516_POLE_RA       = (  268.05     -0.009       0.  )
        BODY516_POLE_DEC      = (   64.49      0.003       0.  )
        BODY516_PM            = (  346.09   1221.2547301   0.  )
        BODY516_LONG_AXIS     = (    0.                        )
 
        \begintext
 
 
 
Satellites of Saturn
      
     
     Mimas
 
        Old values:
        
           Values are unchanged in the 2006 IAU report.  
               
        Current values:
 
        \begindata
  
           BODY601_POLE_RA       = (   40.66     -0.036      0.  )
           BODY601_POLE_DEC      = (   83.52     -0.004      0.  )
           BODY601_PM            = (  337.46    381.9945550  0.  )
           BODY601_LONG_AXIS     = (     0.                      )
 
           BODY601_NUT_PREC_RA   = ( 0. 0.   13.56  0.    0.    0. 0. 0. 0. )
           BODY601_NUT_PREC_DEC  = ( 0. 0.   -1.53  0.    0.    0. 0. 0. 0. )
           BODY601_NUT_PREC_PM   = ( 0. 0.  -13.48  0.  -44.85  0. 0. 0. 0. )

        \begintext
 
 
     Enceladus
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report.  
               
        Current values:
 
        \begindata
 
           BODY602_POLE_RA       = (   40.66    -0.036       0. )
           BODY602_POLE_DEC      = (   83.52    -0.004       0. )
           BODY602_PM            = (    2.82   262.7318996   0. )
           BODY602_LONG_AXIS     = (    0.                      )

        \begintext
 
 
 
     Tethys
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 
 
        Current values:
 
        \begindata
 
           BODY603_POLE_RA       = (   40.66    -0.036       0. )
           BODY603_POLE_DEC      = (   83.52    -0.004       0. )
           BODY603_PM            = (   10.45   190.6979085   0. )
           BODY603_LONG_AXIS     = (    0.                      )
 
           BODY603_NUT_PREC_RA   = ( 0. 0. 0.   9.66   0.    0.  0.  0.  0. )
           BODY603_NUT_PREC_DEC  = ( 0. 0. 0.  -1.09   0.    0.  0.  0.  0. )
           BODY603_NUT_PREC_PM   = ( 0. 0. 0.  -9.60   2.23  0.  0.  0.  0. )

        \begintext
 
 
     Dione
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 
 
        Current values:
 
        \begindata
   
           BODY604_POLE_RA       = (  40.66      -0.036      0.  )
           BODY604_POLE_DEC      = (  83.52      -0.004      0.  )
           BODY604_PM            = (  357.00    131.5349316  0.  )
           BODY604_LONG_AXIS     = (    0.                       )

        \begintext
 
 
 
     Rhea
     
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 
 
        Current values:
 
        \begindata
   
           BODY605_POLE_RA       = (   40.38   -0.036       0. )
           BODY605_POLE_DEC      = (   83.55   -0.004       0. )
           BODY605_PM            = (  235.16   79.6900478   0. )
           BODY605_LONG_AXIS     = (    0.                     )
 
           BODY605_NUT_PREC_RA   = ( 0. 0. 0. 0. 0.   3.10   0. 0. 0. )
           BODY605_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0.  -0.35   0. 0. 0. )
           BODY605_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  -3.08   0. 0. 0. )
 
        \begintext
 
 
 
     Titan
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 
           BODY606_POLE_RA       = (    36.41   -0.036      0. )
           BODY606_POLE_DEC      = (    83.94   -0.004      0. )
           BODY606_PM            = (   189.64   22.5769768  0. )
           BODY606_LONG_AXIS     = (     0.                    )
 
           BODY606_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 0.  2.66  0. 0 )
           BODY606_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 0. -0.30  0. 0 )
           BODY606_NUT_PREC_PM   = ( 0. 0. 0. 0. 0. 0. -2.64  0. 0 )

        \begintext
 
 
 
     Hyperion
 
         The IAU report does not give an orientation model for Hyperion.
         Hyperion's rotation is in chaotic and is not predictable for
         long periods.

 
     Iapetus
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 
           BODY608_POLE_RA       = (   318.16  -3.949      0.  )
           BODY608_POLE_DEC      = (    75.03  -1.143      0.  )
           BODY608_PM            = (   350.20   4.5379572  0.  )
           BODY608_LONG_AXIS     = (     0.                    )

        \begintext
 
 
 
     Phoebe
 

        Old values:
        
           Values are from the 2003 IAU report. 
  
           body609_pole_ra       = ( 355.00       0.         0.  )
           body609_pole_dec      = (  68.70       0.         0.  )
           body609_pm            = ( 304.70     930.8338720  0.  )
           body609_long_axis     = (    0.                       )

        Current values:
 
        \begindata 
  
           BODY609_POLE_RA       = ( 356.90       0.         0.  )
           BODY609_POLE_DEC      = (  77.80       0.         0.  )
           BODY609_PM            = ( 178.58     931.639      0.  )
           BODY609_LONG_AXIS     = (    0.                       )

        \begintext
 
 
     Janus
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata

           BODY610_POLE_RA       = (  40.58    -0.036       0. )
           BODY610_POLE_DEC      = (  83.52    -0.004       0. )
           BODY610_PM            = (  58.83   518.2359876   0. )
           BODY610_LONG_AXIS     = (   0.                      )
 
           BODY610_NUT_PREC_RA   = ( 0. -1.623  0. 0. 0. 0. 0. 0.  0.023 )
           BODY610_NUT_PREC_DEC  = ( 0. -0.183  0. 0. 0. 0. 0. 0.  0.001 )
           BODY610_NUT_PREC_PM   = ( 0.  1.613  0. 0. 0. 0. 0. 0. -0.023 )
 
        \begintext
 
 
 
     Epimetheus
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 
         
        Current values:
 
        \begindata 
  
           BODY611_POLE_RA       = (  40.58    -0.036        0. )
           BODY611_POLE_DEC      = (  83.52    -0.004        0. )
           BODY611_PM            = ( 293.87   518.4907239    0. )
           BODY611_LONG_AXIS     = (   0.                       )
 
           BODY611_NUT_PREC_RA   = ( -3.153   0. 0. 0. 0. 0. 0.   0.086  0. )
           BODY611_NUT_PREC_DEC  = ( -0.356   0. 0. 0. 0. 0. 0.   0.005  0. )
           BODY611_NUT_PREC_PM   = (  3.133   0. 0. 0. 0. 0. 0.  -0.086  0. )

        \begintext
 
 
 
     Helene
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata 
 
           BODY612_POLE_RA       = (  40.85     -0.036        0. )
           BODY612_POLE_DEC      = (  83.34     -0.004        0. )
           BODY612_PM            = ( 245.12    131.6174056    0. )
           BODY612_LONG_AXIS     = (   0.                        )

        \begintext
 
 
 
     Telesto
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata 
 
           BODY613_POLE_RA       = ( 50.51    -0.036      0.  )
           BODY613_POLE_DEC      = ( 84.06    -0.004      0.  )
           BODY613_PM            = ( 56.88   190.6979332  0.  )
           BODY613_LONG_AXIS     = (  0.                      )

        \begintext

 
 
     Calypso
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
  
           BODY614_POLE_RA       = (   36.41    -0.036        0.  )
           BODY614_POLE_DEC      = (   85.04    -0.004        0.  )
           BODY614_PM            = (  153.51   190.6742373    0.  )
           BODY614_LONG_AXIS     = (    0.                        )
 
        \begintext
 
 
 
     Atlas
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 
           BODY615_POLE_RA       = (   40.58     -0.036      0. )
           BODY615_POLE_DEC      = (   83.53     -0.004      0. )  
           BODY615_PM            = (  137.88    598.3060000  0. )
           BODY615_LONG_AXIS     = (    0.                      )

        \begintext
 
 
 
     Prometheus
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
  
           BODY616_POLE_RA       = (  40.58      -0.036    )
           BODY616_POLE_DEC      = (  83.53      -0.004    )
           BODY616_PM            = ( 296.14     587.289000 )
           BODY616_LONG_AXIS     = (   0.                  )
 
        \begintext
 
 
 
     Pandora
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 
           BODY617_POLE_RA       = (   40.58     -0.036      0.  )
           BODY617_POLE_DEC      = (   83.53     -0.004      0.  )
           BODY617_PM            = (  162.92    572.7891000  0.  )
           BODY617_LONG_AXIS     = (     0.                      )
 
        \begintext
 
 
 
     Pan
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 
           BODY618_POLE_RA       = (   40.6     -0.036       0. )
           BODY618_POLE_DEC      = (   83.5     -0.004       0. )
           BODY618_PM            = (   48.8    626.0440000   0. )
           BODY618_LONG_AXIS     = (    0.                      )

        \begintext
 
 
 
 
 
Satellites of Uranus
 
  
 
     Ariel
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 
 
        Current values:

        \begindata 

           BODY701_POLE_RA       = ( 257.43     0.          0. )
           BODY701_POLE_DEC      = ( -15.10     0.          0. )
           BODY701_PM            = ( 156.22  -142.8356681   0. )
           BODY701_LONG_AXIS     = (   0.                      )
 
           BODY701_NUT_PREC_RA   = (  0. 0. 0. 0. 0.
                                      0. 0. 0. 0. 0.  0.    0.    0.29 )
 
           BODY701_NUT_PREC_DEC  = (  0. 0. 0. 0. 0.
                                      0. 0. 0. 0. 0.  0.    0.    0.28 )
 
           BODY701_NUT_PREC_PM   = (  0. 0. 0. 0. 0.
                                      0. 0. 0. 0. 0.  0.   0.05   0.08 )
        \begintext
 
 
 
     Umbriel
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata 
 
           BODY702_POLE_RA       = (  257.43     0.          0. )
           BODY702_POLE_DEC      = (  -15.10     0.          0. )
           BODY702_PM            = (  108.05   -86.8688923   0. )
           BODY702_LONG_AXIS     = (    0.                      )
 
           BODY702_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
                                     0. 0. 0. 0. 0.   0.   0.    0.   0.21 )
 
           BODY702_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
                                     0. 0. 0. 0. 0.   0.   0.    0.   0.20 )
 
           BODY702_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
                                     0. 0. 0. 0. 0.   0.  -0.09  0.   0.06 )

        \begintext
 
 
 
     Titania
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 
           BODY703_POLE_RA       = (  257.43    0.          0. )
           BODY703_POLE_DEC      = (  -15.10    0.          0. )
           BODY703_PM            = (   77.74  -41.3514316   0. )
           BODY703_LONG_AXIS     = (    0.                     )
 
           BODY703_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.29 )
 
           BODY703_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.28 )
 
           BODY703_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
                                     0. 0. 0. 0. 0.   0. 0. 0. 0.   0.08 )
        \begintext
 
 
 
     Oberon
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
  
           BODY704_POLE_RA       = (  257.43    0.          0. )
           BODY704_POLE_DEC      = (  -15.10    0.          0. )
           BODY704_PM            = (    6.77  -26.7394932   0. )
           BODY704_LONG_AXIS     = (    0.                     )
 
 
           BODY704_NUT_PREC_RA   = ( 0. 0. 0. 0. 0. 
                                     0. 0. 0. 0. 0. 
                                     0. 0. 0. 0. 0.   0.16 )
 
           BODY704_NUT_PREC_DEC  = ( 0. 0. 0. 0. 0. 
                                     0. 0. 0. 0. 0. 
                                     0. 0. 0. 0. 0.   0.16 )
 
           BODY704_NUT_PREC_PM   = ( 0. 0. 0. 0. 0.  
                                     0. 0. 0. 0. 0.  
                                     0. 0. 0. 0. 0.   0.04 )
        \begintext
 
 
 
     Miranda
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 

           BODY705_POLE_RA      = (  257.43     0.         0. )
           BODY705_POLE_DEC     = (  -15.08     0.         0. )
           BODY705_PM           = (   30.70  -254.6906892  0. )
           BODY705_LONG_AXIS    = (    0.                     )
 
           BODY705_NUT_PREC_RA  = ( 0.     0.     0.    0.    0.  
                                    0.     0.     0.    0.    0. 
                                    4.41   0.     0.    0.    0. 
                                    0.    -0.04   0.             )
 
           BODY705_NUT_PREC_DEC = ( 0.     0.     0.    0.    0.  
                                    0.     0.     0.    0.    0. 
                                    4.25   0.     0.    0.    0. 
                                    0.    -0.02   0.             )
 
           BODY705_NUT_PREC_PM  = ( 0.     0.     0.    0.    0.  
                                    0.     0.     0.    0.    0. 
                                    1.15  -1.27   0.    0.    0.  
                                    0.    -0.09   0.15           )
        \begintext
 
 
 
     Cordelia
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
  
           BODY706_POLE_RA      = (   257.31      0.         0.  )
           BODY706_POLE_DEC     = (   -15.18      0.         0.  )
           BODY706_PM           = (   127.69  -1074.5205730  0.  )
           BODY706_LONG_AXIS    = (     0.                       )
 
           BODY706_NUT_PREC_RA  = (   -0.15    0.     0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.             )

           BODY706_NUT_PREC_DEC = (    0.14    0.     0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.             )  

           BODY706_NUT_PREC_PM  = (   -0.04    0.     0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.             ) 
 
        \begintext
 
 

     Ophelia
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
   
           BODY707_POLE_RA      = (  257.31     0.         0. )
           BODY707_POLE_DEC     = (  -15.18     0.         0. )
           BODY707_PM           = (  130.35  -956.4068150  0. )
           BODY707_LONG_AXIS    = (    0.                     )
 
           BODY707_NUT_PREC_RA  = (    0.     -0.09   0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.             )

           BODY707_NUT_PREC_DEC = (    0.      0.09   0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.             )

           BODY707_NUT_PREC_PM  = (    0.     -0.03   0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.    0.    0.
                                       0.      0.     0.             )
 
        \begintext
 
 
 
     Bianca
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 
           BODY708_POLE_RA      = (  257.31     0.         0.  )
           BODY708_POLE_DEC     = (  -15.18     0.         0.  )
           BODY708_PM           = (  105.46  -828.3914760  0.  )
           BODY708_LONG_AXIS    = (    0.                      )
 
           BODY708_NUT_PREC_RA  = (    0.      0.    -0.16    0.    0.
                                       0.      0.     0.      0.    0.
                                       0.      0.     0.      0.    0.
                                       0.      0.     0.               )

           BODY708_NUT_PREC_DEC = (    0.      0.     0.16    0.    0.
                                       0.      0.     0.      0.    0.
                                       0.      0.     0.      0.    0.
                                       0.      0.     0.               )

           BODY708_NUT_PREC_PM  = (    0.      0.    -0.04    0.    0.
                                       0.      0.     0.      0.    0.
                                       0.      0.     0.      0.    0.
                                       0.      0.     0.               )

        \begintext
 
 
 
     Cressida
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 
 
           BODY709_POLE_RA      = (  257.31      0.          0.  )
           BODY709_POLE_DEC     = (  -15.18      0.          0.  )
           BODY709_PM           = (   59.16   -776.5816320   0.  )
           BODY709_LONG_AXIS    = (    0.                        )
 

           BODY709_NUT_PREC_RA  = (    0.      0.     0.     -0.04   0.
                                       0.      0.     0.      0.     0.
                                       0.      0.     0.      0.     0.
                                       0.      0.     0.                )


           BODY709_NUT_PREC_DEC = (    0.      0.     0.      0.04   0.
                                       0.      0.     0.      0.     0.
                                       0.      0.     0.      0.     0.
                                       0.      0.     0.                )


           BODY709_NUT_PREC_PM  = (    0.      0.     0.     -0.01   0.
                                       0.      0.     0.      0.     0.
                                       0.      0.     0.      0.     0.
                                       0.      0.     0.                )


        \begintext
 
 
 
     Desdemona
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata 
  
           BODY710_POLE_RA      = ( 257.31      0.           0.  )
           BODY710_POLE_DEC     = ( -15.18      0.           0.  )
           BODY710_PM           = (  95.08   -760.0531690    0.  )
           BODY710_LONG_AXIS    = (   0.                         )
 
           BODY710_NUT_PREC_RA  = (   0.      0.     0.      0.    -0.17 
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                  )

           BODY710_NUT_PREC_DEC = (   0.      0.     0.      0.     0.16 
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                  )

           BODY710_NUT_PREC_PM  = (   0.      0.     0.      0.    -0.04  
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                 )

        \begintext
 
 
 
     Juliet
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
  
           BODY711_POLE_RA      = (  257.31     0.           0.   )
           BODY711_POLE_DEC     = (  -15.18     0.           0.   )
           BODY711_PM           = (  302.56  -730.1253660    0.   )
           BODY711_LONG_AXIS    = (    0.                         )
 
           BODY711_NUT_PREC_RA  = (   0.      0.     0.      0.     0.  
                                     -0.06    0.     0.      0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                 )
 
           BODY711_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
                                      0.06    0.     0.      0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                 )
  
           BODY711_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
                                     -0.02    0.     0.      0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                 )
 
        \begintext
 
 
 
     Portia
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
    
           BODY712_POLE_RA      = (  257.31      0.           0.   )
           BODY712_POLE_DEC     = (  -15.18      0.           0.   )
           BODY712_PM           = (   25.03   -701.4865870    0.   )
           BODY712_LONG_AXIS    = (    0.                          )
 
           BODY712_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
                                      0.     -0.09   0.      0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                )

           BODY712_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
                                      0.      0.09   0.      0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.               )

           BODY712_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
                                      0.     -0.02   0.      0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.               )

        \begintext
 
 
 
     Rosalind
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
   
           BODY713_POLE_RA      = ( 257.31      0.          0.  )
           BODY713_POLE_DEC     = ( -15.18      0.          0.  )
           BODY713_PM           = ( 314.90   -644.6311260   0.  )
           BODY713_LONG_AXIS    = (   0.                        )
 
           BODY713_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
                                      0.      0.    -0.29    0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.               )

           BODY713_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
                                      0.      0.     0.28    0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.              )

           BODY713_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
                                      0.      0.    -0.08    0.     0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.              )
 
        \begintext
 
 
 
     Belinda
 
       Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata 
 
           BODY714_POLE_RA      = (   257.31      0.         0. )
           BODY714_POLE_DEC     = (   -15.18      0.         0. )
           BODY714_PM           = (   297.46   -577.3628170  0. )
           BODY714_LONG_AXIS    = (     0.                      )
 
           BODY714_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
                                      0.      0.     0.     -0.03   0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                )

           BODY714_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
                                      0.      0.     0.      0.03   0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                )

           BODY714_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
                                      0.      0.     0.     -0.01   0.
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                )
        \begintext
 
 
 
     Puck
 
       Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
  
           BODY715_POLE_RA      = (  257.31      0.         0.  )
           BODY715_POLE_DEC     = (  -15.18      0.         0.  )
           BODY715_PM           = (   91.24   -472.5450690  0.  )
           BODY715_LONG_AXIS    = (    0.                       )
 
           BODY715_NUT_PREC_RA  = (   0.      0.     0.      0.     0. 
                                      0.      0.     0.      0.    -0.33 
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                  )

           BODY715_NUT_PREC_DEC = (   0.      0.     0.      0.     0. 
                                      0.      0.     0.      0.     0.31
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                  )

           BODY715_NUT_PREC_PM  = (   0.      0.     0.      0.     0. 
                                      0.      0.     0.      0.    -0.09
                                      0.      0.     0.      0.     0.
                                      0.      0.     0.                  )
  
        \begintext
 
 
 
 
Satellites of Neptune
 
 
     Triton
 
       Old values:
        
           Values are unchanged in the 2006 IAU report. 
 
        Current values:
 
        \begindata

           BODY801_POLE_RA       = ( 299.36     0.         0.  )
           BODY801_POLE_DEC      = (  41.17     0.         0.  )
           BODY801_PM            = ( 296.53   -61.2572637  0.  )
           BODY801_LONG_AXIS     = (   0.                      )
 
 
           BODY801_NUT_PREC_RA   = (  0.      0.      0.      0.  
                                      0.      0.      0.    -32.35    
                                      0.     -6.28   -2.08   -0.74       
                                     -0.28   -0.11   -0.07   -0.02    
                                     -0.01                         )
 
 
           BODY801_NUT_PREC_DEC  = (  0.      0.      0.      0.  
                                      0.      0.      0.     22.55    
                                      0.      2.10    0.55    0.16   
                                      0.05    0.02    0.01    0.
                                      0.                           )
 
 
           BODY801_NUT_PREC_PM   = (  0.      0.      0.      0.  
                                      0.      0.      0.     22.25   
                                      0.      6.73    2.05    0.74   
                                      0.28    0.11    0.05    0.02
                                      0.01                         )
  
        \begintext
 
 
 
 
     Nereid
 
        Old values:
 
           Values are from the 1988 IAU report [10].  Note that this 
           rotation model pre-dated the 1989 Voyager 2 Neptune
           encounter.

 
           body802_pole_ra       = (    273.48    0.        0.  )
           body802_pole_dec      = (     67.22    0.        0.  )
           body802_pm            = (    237.22    0.9996465 0.  )
           body802_long_axis     = (      0.                    )
 
 
           The report seems to have a typo:  in the nut_prec_ra expression,
           where the report gives  -0.51 sin 3N3, we use -0.51 3N2.
 
           body802_nut_prec_ra   = (  0.    -17.81
                                      0.      0.     0.      0.
                                      0.      0.     0.
                                      2.56   -0.51   0.11   -0.03  )
 
           body802_nut_prec_dec  = (  0.     -6.67
                                      0.      0.     0.      0.
                                      0.      0.     0.
                                      0.47   -0.07   0.01          )
 
           body802_nut_prec_pm   = (  0.     16.48
                                      0.      0.     0.      0.
                                      0.      0.     0.
                                     -2.57    0.51 -0.11    0.02  )
 
 
 
        Current values:
 
           The 2006 report [1] states that values for Nereid are not
           given because Nereid is not in synchronous rotation with Neptune
           (p. 167).
 
 
 
     Naiad
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
 
        \begindata
  
           BODY803_POLE_RA       = (  299.36      0.          0.  )
           BODY803_POLE_DEC      = (   43.36      0.          0.  )
           BODY803_PM            = (  254.06  +1222.8441209   0.  )
           BODY803_LONG_AXIS     = (    0.                        )
 
 
           BODY803_NUT_PREC_RA   = (    0.70     -6.49     0.      0.
                                        0.        0.       0.      0.
                                        0.25      0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                            )
 
           BODY803_NUT_PREC_DEC  = (   -0.51     -4.75     0.      0.
                                        0.        0.       0.      0.
                                        0.09      0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                            )
 
           BODY803_NUT_PREC_PM   = (   -0.48      4.40     0.      0.
                                        0.        0.       0.      0.
                                       -0.27      0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                            )
    
        \begintext
 
 
 
 
     Thalassa
 

        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata

           BODY804_POLE_RA       = (  299.36      0.          0. )
           BODY804_POLE_DEC      = (   43.45      0.          0. )
           BODY804_PM            = (  102.06   1155.7555612   0. )  
           BODY804_LONG_AXIS     = (    0.                       )
 
 
           BODY804_NUT_PREC_RA   = (    0.70      0.      -0.28    0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                             )
   
  
           BODY804_NUT_PREC_DEC  = (   -0.51      0.      -0.21    0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0. 
                                        0.                             )
 
           BODY804_NUT_PREC_PM   = (   -0.48      0.       0.19    0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0. 
                                        0.                             )
                                                                 
        \begintext
 
 
 
     Despina
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
 
        \begindata
  
           BODY805_POLE_RA       = (  299.36      0.          0. )
           BODY805_POLE_DEC      = (   43.45      0.          0. )
           BODY805_PM            = (  306.51  +1075.7341562   0. )
           BODY805_LONG_AXIS     = (    0.                       )
 
 
           BODY805_NUT_PREC_RA   = (    0.70      0.       0.     -0.09
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                              )
 
           BODY805_NUT_PREC_DEC  = (   -0.51      0.       0.     -0.07
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                              )
 
           BODY805_NUT_PREC_PM   = (   -0.49      0.       0.      0.06
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                              )
        \begintext
 
 
 
     Galatea
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
 
        \begindata
  
           BODY806_POLE_RA       = (   299.36      0.          0. )
           BODY806_POLE_DEC      = (    43.43      0.          0. )
           BODY806_PM            = (   258.09    839.6597686   0. )
           BODY806_LONG_AXIS     = (     0.                       )
 
 
           BODY806_NUT_PREC_RA   = (    0.70      0.       0.      0.
                                       -0.07      0.       0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                             )
 
           BODY806_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
                                       -0.05      0.       0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                             )
 
           BODY806_NUT_PREC_PM   = (   -0.48      0.       0.      0.
                                        0.05      0.       0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                             ) 
        \begintext

 
     Larissa
 
 
        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
  
        \begindata

           BODY807_POLE_RA       = (   299.36     0.           0. )
           BODY807_POLE_DEC      = (    43.41     0.           0. )
           BODY807_PM            = (   179.41  +649.0534470    0. )
           BODY807_LONG_AXIS     = (     0.                       )
 
 
           BODY807_NUT_PREC_RA   = (    0.70      0.       0.      0.
                                        0.       -0.27     0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                            )
 
           BODY807_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
                                        0.       -0.20     0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                            )
 
           BODY807_NUT_PREC_PM   = (   -0.48      0.       0.      0.
                                        0.        0.19     0.      0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                            )
        \begintext
 
 
 
     Proteus
 

        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata

           BODY808_POLE_RA       = (  299.27      0.          0.  )
           BODY808_POLE_DEC      = (   42.91      0.          0.  )
           BODY808_PM            = (   93.38   +320.7654228   0.  )
           BODY808_LONG_AXIS     = (    0.                        )
 
 
           BODY808_NUT_PREC_RA   = (    0.70      0.       0.      0.
                                        0.        0.      -0.05    0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                             )
 
           BODY808_NUT_PREC_DEC  = (   -0.51      0.       0.      0.
                                        0.        0.      -0.04    0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                             )
 
           BODY808_NUT_PREC_PM   = (   -0.48      0.       0.      0.
                                        0.        0.       0.04    0.
                                        0.        0.       0.      0.
                                        0.        0.       0.      0.
                                        0.                             )
   
        \begintext
  
 
 
 
 
Satellites of Pluto
 
     Charon
 
        Old values:
        
           Values are from the 2003 IAU report. 
 
           body901_pole_ra       = (   313.02     0.         0. )
           body901_pole_dec      = (     9.09     0.         0. )
           body901_pm            = (    56.77   -56.3623195  0. )
           body901_long_axis     = (     0.                     )
               
        Current values:
 
        \begindata
 
           BODY901_POLE_RA       = (   312.993    0.         0. )
           BODY901_POLE_DEC      = (     6.163    0.         0. )
           BODY901_PM            = (    57.305  -56.3625225  0. )
           BODY901_LONG_AXIS     = (     0.                     )

        \begintext
 
 
 
Orientation constants for Selected Comets and Asteroids
--------------------------------------------------------



19P/Borrelly


        Current values:
 
        \begindata

           BODY1000005_POLE_RA       = (   218.5      0.         0.  )
           BODY1000005_POLE_DEC      = (   -12.5      0.         0.  )
           BODY1000005_PM            = (   000.     390.0        0.  )
           BODY1000005_LONG_AXIS     = (     0.                      )
 
        \begintext



9P/Tempel 1


        Current values:
 
        \begindata

           BODY1000093_POLE_RA       = (   294.       0.         0.  )
           BODY1000093_POLE_DEC      = (    73.       0.         0.  )
           BODY1000093_PM            = (   252.63   212.064      0.  )
           BODY1000093_LONG_AXIS     = (     0.                      )
 
        \begintext


Vesta

        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata

           BODY2000004_POLE_RA       = (   301.      0.         0.  )
           BODY2000004_POLE_DEC      = (    41.      0.         0.  )
           BODY2000004_PM            = (   292.   1617.332776   0.  )
           BODY2000004_LONG_AXIS     = (     0.                     )
 
        \begintext

Eros

        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata

           BODY2000433_POLE_RA       = (   11.35       0.           0. )
           BODY2000433_POLE_DEC      = (   17.22       0.           0. )
           BODY2000433_PM            = (  326.07    1639.38864745   0. )
           BODY2000433_LONG_AXIS     = (    0.                         )
 
        \begintext


Itokawa


        Current values:
 
        \begindata

           BODY2025143_POLE_RA       = (   90.53       0.           0. )
           BODY2025143_POLE_DEC      = (  -66.30       0.           0. )
           BODY2025143_PM            = (  000.0      712.143        0. )
           BODY2025143_LONG_AXIS     = (    0.                         )
 
        \begintext



Ida

        Old values:
        
           Values are unchanged in the 2006 IAU report. 

        Current values:
 
        \begindata
 
           BODY2431010_POLE_RA       = (  168.76      0.         0. )
           BODY2431010_POLE_DEC      = (   -2.88      0.         0. )
           BODY2431010_PM            = (  265.95  +1864.6280070  0. )
           BODY2431010_LONG_AXIS     = (    0.                      )
 
        \begintext

Gaspra

        Old values:
        
           Values are unchanged in the 2006 IAU report. 
               
        Current values:
 
        \begindata 
 
           BODY9511010_POLE_RA       = (   9.47     0.         0. )
           BODY9511010_POLE_DEC      = (  26.70     0.         0. )
           BODY9511010_PM            = (  83.67  1226.9114850  0. )
           BODY9511010_LONG_AXIS     = (   0.                     )

        \begintext









 
Radii of Sun and Planets
--------------------------------------------------------
 
 
Sun
 
     Value for the Sun is from the [3], page K7.
 
        \begindata
 
        BODY10_RADII      = (   696000.     696000.      696000.     )
 
        \begintext
 
 
Mercury
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
 
     Current values:
 
        \begindata
 
        BODY199_RADII     = ( 2439.7   2439.7   2439.7 )
 
        \begintext
 
 
Venus
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
 
     Current values:
 
        \begindata
 
        BODY299_RADII     = ( 6051.8   6051.8   6051.8 )
 
        \begintext
 
 
Earth
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
 
     Current values:
 

        \begindata
 
        BODY399_RADII     = ( 6378.14   6378.14   6356.75 )
 
        \begintext
 
 
Mars
 
 
     Old values:

        body499_radii       = (     3397.      3397.         3375.     )
 
     Current values:


        The IAU report gives separate values for the north and south
        polar radii:

           north:  3373.19
           south:  3379.21 

        We use the average of these values as the polar radius for
        the triaxial model.
 
        \begindata
 
        BODY499_RADII       = ( 3396.19   3396.19   3376.20 )
 
        \begintext
 
 
 
Jupiter
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
 
     Current values:
 
        \begindata
 
        BODY599_RADII     = ( 71492   71492   66854 )
 
        \begintext
 
 
 
Saturn
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
 
     Current values:
 
        \begindata
 
        BODY699_RADII     = ( 60268   60268   54364 )
 
        \begintext
 
 
 
Uranus
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
 
     Current values:
 
        \begindata
 
        BODY799_RADII     = ( 25559   25559   24973 )
 
        \begintext
 
 
 
Neptune
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
  
     Current values:
 
        (Values are for the 1 bar pressure level.)
 
        \begindata
 
        BODY899_RADII     = ( 24764   24764  24341 )
 
        \begintext
 
 
 
Pluto
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
 
     Current values:
 
        \begindata
 
        BODY999_RADII     = ( 1195   1195   1195 )
 
        \begintext
 



Radii of Satellites
--------------------------------------------------------
 
 
Moon
 
     Old values:
 
        Values are unchanged in the 2006 IAU report. 
 
     Current values:
 
        \begindata
 
        BODY301_RADII     = ( 1737.4   1737.4   1737.4 )
 
        \begintext
 
 
 
Satellites of Mars
 
     Old values:
 
        Values are unchanged in the 2006 IAU report. 
 
     Current values:
 
        \begindata
 
        BODY401_RADII     = ( 13.4    11.2    9.2 )
        BODY402_RADII     = (  7.5     6.1    5.2 )
 
        \begintext
 
 
 
Satellites of Jupiter
 
     Old values:
 
        Values are unchanged in the 2006 IAU report.
 
     Current values:
         
        \begindata
 
        BODY501_RADII     = ( 1829.4   1819.3   1815.7  )
        BODY502_RADII     = ( 1564.13  1561.23  1560.93 )
        BODY503_RADII     = ( 2632.4   2632.29  2632.35 )
        BODY504_RADII     = ( 2409.4   2409.2   2409.3  )
        BODY505_RADII     = (  125       73       64    )
 
        \begintext
 
        Only mean radii are available in the 2003 IAU report for bodies
        506-513.
 
        \begindata
 
        BODY506_RADII    = (    85       85       85   )
        BODY507_RADII    = (    40       40       40   )
        BODY508_RADII    = (    18       18       18   )
        BODY509_RADII    = (    14       14       14   )
        BODY510_RADII    = (    12       12       12   )
        BODY511_RADII    = (    15       15       15   )
        BODY512_RADII    = (    10       10       10   )
        BODY513_RADII    = (     5        5        5   )
        BODY514_RADII    = (    58       49       42   )
        BODY515_RADII    = (    10        8        7   )
 
        \begintext
 
        The value for the second radius for body 516 is not given in 
        2003 IAU report.   The values given are:
 
           BODY516_RADII    = (  30   ---   20   )
 
        For use within the SPICE system, we use only the mean radius.
        \begindata
 
        BODY516_RADII    = (  21.5   21.5  21.5  )
 
        \begintext
 
 
 
Satellites of Saturn
 
 
     Old values:
 
        Values are from the 2003 IAU report.
    
        body601_radii     = (  209.1   196.2   191.4 )
        body602_radii     = (  256.3   247.3   244.6 )
        body603_radii     = (  535.6   528.2   525.8 )
        body604_radii     = (  560     560     560   )
        body605_radii     = (  764     764     764   )
        body606_radii     = ( 2575    2575    2575   )
        body607_radii     = (  164     130     107   )
        body608_radii     = (  718     718     718   )
        body609_radii     = (  115     110     105   )
        body610_radii     = (   97.0    95.0    77.0 )
        body611_radii     = (   69.0    55.0    55.0 )
 
 
        Only the first equatorial radius for Helene (body 612) was given in the
        2003 IAU report:
 
            body612_radii     = (       17.5        ---          ---     )
 
        The mean radius was 16km; we used this radius for all three axes, as
        we do for the satellites for which only the mean radius is available.
 
 
        body612_radii     = (   16      16       16  )
        body613_radii     = (   15      12.5     7.5 )
        body614_radii     = (   15.0     8.0     8.0 )
        body615_radii     = (   18.5    17.2    13.5 )
        body616_radii     = (   74.0    50.0    34.0 )
        body617_radii     = (   55.0    44.0    31.0 )
  
      
 
     Current values:
 
        \begindata
 
        BODY601_RADII     = (  207.4     196.8     190.6  )
        BODY602_RADII     = (  256.6     251.4     248.3  )
        BODY603_RADII     = (  540.4     531.1     527.5  )
        BODY604_RADII     = (  563.8     561.0     560.3  )
        BODY605_RADII     = (  767.2     762.5     763.1  )
        BODY606_RADII     = ( 2575      2575      2575    )
        BODY607_RADII     = (  164       130       107    )
        BODY608_RADII     = (  747.4     747.4     712.4  )
        BODY609_RADII     = (  108.6     107.7     101.5  )
        BODY610_RADII     = (   97.0      95.0      77.0  )
        BODY611_RADII     = (   69.0      55.0      55.0  )
 
        \begintext
 
        Only the first equatorial radius for Helene (body 612) is given in the
        2006 IAU report:
 
            BODY612_RADII     = (       17.5        ---          ---     )
 
        The mean radius is 16km; we use this radius for all three axes, as
        we do for the satellites for which only the mean radius is available.
 
 
        \begindata
 
        BODY612_RADII     = (  17.5      17.5      17.5  )
        BODY613_RADII     = (  15        12.5       7.5  )
        BODY614_RADII     = (  15.0       8.0       8.0  )
        BODY615_RADII     = (  18.5      17.2      13.5  )
        BODY616_RADII     = (  74.0      50.0      34.0  )
        BODY617_RADII     = (  55.0      44.0      31.0  )
 
        \begintext
 
 
         For Pan, only a mean radius is given in the 2006 report.
 
        \begindata
 
        BODY618_RADII     = (   10       10     10   )
 
        \begintext
 
 
 
Satellites of Uranus
 
     Old values:
 
        Values are unchanged in the 2006 IAU report. 
 
     Current values:
 
        \begindata
 
        BODY701_RADII     = (  581.1   577.9   577.7 )
        BODY702_RADII     = (  584.7   584.7   584.7 )
        BODY703_RADII     = (  788.9   788.9   788.9 )
        BODY704_RADII     = (  761.4   761.4   761.4 )
        BODY705_RADII     = (  240.4   234.2   232.9 )
 
        \begintext
 
        The 2000 report gives only mean radii for satellites 706--715.
 
        \begindata
 
        BODY706_RADII     = (   13      13      13 )
        BODY707_RADII     = (   15      15      15 )
        BODY708_RADII     = (   21      21      21 )
        BODY709_RADII     = (   31      31      31 )
        BODY710_RADII     = (   27      27      27 )
        BODY711_RADII     = (   42      42      42 )
        BODY712_RADII     = (   54      54      54 )
        BODY713_RADII     = (   27      27      27 )
        BODY714_RADII     = (   33      33      33 )
        BODY715_RADII     = (   77      77      77 )
 
        \begintext
 
 
 
 
Satellites of Neptune
 
 
     Old values:
 
        Values are unchanged in the 2006 IAU report. 
 
     Current values:
 
        The 2000 report gives mean radii only for bodies 801-806.
 
        \begindata
 
        BODY801_RADII     = ( 1352.6  1352.6  1352.6 )
        BODY802_RADII     = (  170     170     170   )
        BODY803_RADII     = (   29      29     29    )
        BODY804_RADII     = (   40      40     40    )
        BODY805_RADII     = (   74      74     74    )
        BODY806_RADII     = (   79      79     79    )
 
        \begintext
 
 
        The second equatorial radius for Larissa is not given in the 2000
        report.  The available values are:
 
            BODY807_RADII     = (   104     ---     89   )
 
        For use within the SPICE system, we use only the mean radius.
        \begindata
 
        BODY807_RADII     = (   96      96     96   )
        BODY808_RADII     = (  218     208    201   )
 
        \begintext
 
 
 
 
Satellites of Pluto
 
     
     Old values:
 
        Values are from the 2003 IAU report. 

        BODY901_RADII     = (  593     593    593   )
             
     Current values:
 
        \begindata
 
        BODY901_RADII     = (  605     605    605   )
 
        \begintext
 


Radii for Selected Comets and Asteroids
--------------------------------------------------------


19P/Borrelly


     Current values:
 

        The value in the data assignment below is the 
        "effective radius."

        The first principal axis length is 

           3.5 km

        The lengths of the other semi-axes are not provided
        by [1].

        \begindata
 
        BODY1000005_RADII     = (  4.22   4.22   4.22  )
 
        \begintext



Halley


     Current values:

        \begindata
 
        BODY1000036_RADII     = (  8.0   4.0   4.0  )
 
        \begintext



9P/Tempel 1


     Current values:


        The value in the data assignment below is the 
        "effective radius."
            
        According to [1]:

           The maximum and minimum radii are not properly 
           the values of the principal semi-axes, they
           are half the maximum and minimum values of the
           diameter. Due to the large deviations from a
           simple ellipsoid, they may not correspond with
           measurements along the principal axes, or be
           orthogonal to each other.

        \begindata
 
        BODY1000093_RADII     = (  3.0   3.0   3.0  )
 
        \begintext


81P/Wild 2


     Current values:


        \begindata
 
        BODY1000107_RADII     = (  2.7   1.9   1.5 )
 
        \begintext


Ceres


     Current values:


        \begindata
 
        BODY2000001_RADII     = ( 487.3  487.3  454.7 )
 
        \begintext


Vesta


     Current values:


        \begindata
 
        BODY2000004_RADII     = ( 289.  280.  229.  )
 
        \begintext


Toutatis


     Current values:


        \begindata
 
        BODY2004179_RADII     = (  2.13  1.015  0.85  )
 
        \begintext

 
Kleopatra


     Old values:

        Values are from the 2003 report.

 
        body2000216_radii     = (   108.5      47    40.5  )
 

     Current values:
 
 
        No values are provided in the 2006 report.


Mathilde


     Current values:


        \begindata
 
        BODY2000253_RADII     = (  33.   24.   23.  )
 
        \begintext
       
Eros
 

     Current values:
 
 
        \begindata
 
        BODY2000433_RADII     = (  17.0   5.5   5.5  )
 
        \begintext


Itokawa


     Current values:


        \begindata
 
        BODY2025143_RADII     = (  0.535   0.294   0.209  )
 
        \begintext



Gaspra

     
     Current values:
 
 
        \begindata
 
        BODY9511010_RADII     = (    9.1    5.2    4.4 )
 
        \begintext

        
        
        
Ida

     
     Current values:
 
 
        \begindata
 
        BODY2431010_RADII     = (   26.8   12.0    7.6 )
 
        \begintext

        

===========================================================================
End of file pck00009.tpc
===========================================================================