PDS_VERSION_ID               = PDS3
LABEL_REVISION_NOTE  = "2017-03-13, SONC, version 1.0"
/* PVV version 3.13 */

/* Raw data for both housekeeping and science              */

RECORD_TYPE = UNDEFINED
FILE_RECORDS = 1512
^FILE=("SES_FB1_0809060522.DAT",1<BYTES>)

/* DATA OBJECT POINTERS  */

DATA_SET_ID           = "RL-A-SESAME-1-AST1-V1.0"
DATA_SET_NAME         = "ROSETTA-LANDER STEINS SESAME 1 AST1 V1.0"
PRODUCT_ID            = "SES_FB1_0809060522"
PRODUCT_CREATION_TIME = 2017-03-24T08:56:48
MISSION_NAME           = "INTERNATIONAL ROSETTA MISSION"
MISSION_PHASE_NAME    = "STEINS FLY-BY"
MISSION_ID             = ROSETTA
INSTRUMENT_HOST_NAME   = "ROSETTA-LANDER"
INSTRUMENT_HOST_ID     = RL

PRODUCT_TYPE          = UDR
START_TIME            = 2008-09-06T05:22:35.552
STOP_TIME             = 2008-09-06T06:04:08.552
SPACECRAFT_CLOCK_START_COUNT = "2/179299317.36864"
SPACECRAFT_CLOCK_STOP_COUNT  = "2/179301810.40960"

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           = "2867 STEINS"
TARGET_TYPE           = "ASTEROID"

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

/* GEOMETRY PARAMETERS */

/* SPACECRAFT LOCATION: Position <km> */
SC_SUN_POSITION_VECTOR = (  106573025.4, 270432865.1, 132988157.4)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (     275931.6,    184367.9,     28101.2)
SC_TARGET_VELOCITY_VECTOR = ( 7127.785,4783.324,738.470)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =      333043.2 <km>
SUB_SPACECRAFT_LATITUDE =     6.21 <deg>
SUB_SPACECRAFT_LONGITUDE =   117.35 <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  */



END