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

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

RECORD_TYPE = UNDEFINED
FILE_RECORDS = 2
FILE_NAME = "SES_FS2_DST_0709250458_Z.TAB"

/* DATA OBJECT POINTERS  */

^ST_TABLE = ("SES_FS2_DST_0709250458_Z.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_DST_0709250458_Z"
PRODUCT_CREATION_TIME = 2017-09-01T09:03:07
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            = 2007-09-25T04:58:01.594
STOP_TIME             = 2007-09-25T05:07:01.625
SPACECRAFT_CLOCK_START_COUNT = "2/149317049.13"
SPACECRAFT_CLOCK_STOP_COUNT  = "2/149317589.14"

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 = ( -185091260.7, -34697305.1, -10649863.9)
/* TARGET PARAMETERS: Position <km>, Velocity <m/s> */
SC_TARGET_POSITION_VECTOR = (  -35107499.0, -30738962.9,  -8934398.1)
SC_TARGET_VELOCITY_VECTOR = ( 11646.206,7238.222,2269.779)
/* SPACECRAFT POSITION WITH RESPECT TO CENTRAL BODY */
SPACECRAFT_ALTITUDE =    47504082.5 <km>
SUB_SPACECRAFT_LATITUDE =    10.80 <deg>
SUB_SPACECRAFT_LONGITUDE =   323.88 <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               = ST_TABLE
   NAME               = "ST"
   INTERCHANGE_FORMAT = ASCII
   ROWS               = 2
   COLUMNS            = 11
   ROW_BYTES          = 79
   ^STRUCTURE         = "DIM_ST.FMT"
END_OBJECT           = ST_TABLE



END