PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2017-09-01, SONC, version 1.0"
/* PVV version 3.13 */

/* Edited SC data from DIM Calibration Mode (SONC Level 2) */

RECORD_TYPE = UNDEFINED
FILE_RECORDS = 4
FILE_NAME = "SES_FS2_DCA_0709292212.TAB"

/* DATA OBJECT POINTERS  */

^CAL_TABLE     = ("SES_FS2_DCA_0709292212.TAB",1 <BYTES>)

DATA_SET_ID           = "RL-E-SESAME-2-EAR2-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER EARTH SESAME 2 EAR2 V1.0"
PRODUCT_ID            = "SES_FS2_DCA_0709292212"
PRODUCT_CREATION_TIME = 2017-09-01T09:01:32
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME    = "EARTH SWING-BY 2"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID     = RL

PRODUCT_TYPE          = UDR
START_TIME            = 2007-09-29T22:12:53.606
STOP_TIME             = 2007-09-29T22:21:53.887
SPACECRAFT_CLOCK_START_COUNT = "2/149724741.11"
SPACECRAFT_CLOCK_STOP_COUNT  = "2/149725281.20"

PRODUCER_ID            = "SONC"
PRODUCER_FULL_NAME     = "SCIENCE OPERATIONS AND NAVIGATION CENTER"
PRODUCER_INSTITUTION_NAME = "CNES"

INSTRUMENT_ID          = SESAME
INSTRUMENT_NAME        = "SURFACE ELECTRIC SOUNDING AND
                       ACOUSTIC MONITORING EXPERIMENT"
INSTRUMENT_TYPE        = {"ACOUSTIC SENSOR", "DUST IMPACT DETECTOR",
                       "PERMITTIVITY PROBE"}
TARGET_NAME           = "EARTH"
TARGET_TYPE           = "PLANET"

PROCESSING_LEVEL_ID   = "1"
DATA_QUALITY_ID        = "-1"
DATA_QUALITY_DESC      = "-1 : NOT QUALIFIED"

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = ( -179487300.1, -42775402.3, -14512550.6)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (  -30538893.4, -27750045.6,  -7999628.2)
SC_TARGET_VELOCITY_VECTOR = ( 10772.127,7410.421,2310.378)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =    42025552.1 <km>
SUB_SPACECRAFT_LATITUDE =    10.93 <deg>
SUB_SPACECRAFT_LONGITUDE =    61.50 <deg>
NOTE = "The values of the keywords SC_SUN_POSITION_VECTOR,
       SC_TARGET_POSITION_VECTOR and SC_TARGET_VELOCITY_VECTOR
       are related to the equatorial J2000 inertial frame (EMEJ200).
       The values of SUB_SPACECRAFT_LATITUDE and SUB_SPACECRAFT_LONGITUDE
       are northern latitude and eastern longitude in the standard
       planetocentric IAU_<TARGET_NAME> frame.
       All values are computed for the time = START_TIME.
       Distances are given in <km> velocities in <m/s>, angles in <deg>"

/* DATA OBJECT DEFINITION  */

OBJECT               = CAL_TABLE
   NAME               = "CAL"
   INTERCHANGE_FORMAT = ASCII
   ROWS               = 4
   COLUMNS            = 9
   ROW_BYTES          = 74
   ^STRUCTURE         = "DIM_CA.FMT"
END_OBJECT           = CAL_TABLE



END