PDS_VERSION_ID = PDS3 /*** FILE CHARACTERISTICS ***/ FILE_NAME = "ROS_CAM1_20160416T094721.LBL" RECORD_TYPE = FIXED_LENGTH RECORD_BYTES = 2048 FILE_RECORDS = 1024 INTERCHANGE_FORMAT = BINARY /*** POINTERS TO DATA OBJECTS ***/ ^IMAGE = ("ROS_CAM1_20160416T094721.IMG",1) /*** IDENTIFICATION DATA ELEMENTS ***/ DATA_SET_ID = "RO-C-NAVCAM-2-EXT2-MTP028-V1.0" DATA_SET_NAME = "ROSETTA-ORBITER 67P NAVCAM 2 ROSETTA EXTENSION 2 MTP028 V1.0" PRODUCT_ID = "ROS_CAM1_20160416T094721" PRODUCT_CREATION_TIME = 2016-05-22T20:28:39 PRODUCT_TYPE = EDR PROCESSING_LEVEL_ID = "2" IMAGE_TIME = 2016-04-16T09:47:21.531 START_TIME = 2016-04-16T09:47:21.526 STOP_TIME = 2016-04-16T09:47:21.536 SPACECRAFT_CLOCK_START_COUNT = "1/419420756.44928" SPACECRAFT_CLOCK_STOP_COUNT = "1/419420756.45584" MISSION_ID = "ROSETTA" MISSION_NAME = "INTERNATIONAL ROSETTA MISSION" MISSION_PHASE_NAME = "ROSETTA EXTENSION 2 MTP028" INSTRUMENT_HOST_ID = RO INSTRUMENT_HOST_NAME = "ROSETTA-ORBITER" TARGET_NAME = "67P/CHURYUMOV-GERASIMENKO 1 (1969 R1)" TARGET_TYPE = "COMET" OBSERVATION_TYPE = "NAVIGATION IMAGE" PRODUCER_ID = "ESA-ESAC" PRODUCER_FULL_NAME = "BERNHARD GEIGER" PRODUCER_INSTITUTION_NAME = "EUROPEAN SPACE AGENCY-ESAC" /*** INSTRUMENT RELATED PARAMETERS ***/ INSTRUMENT_ID = NAVCAM INSTRUMENT_NAME = "NAVIGATION CAMERA" INSTRUMENT_TYPE = "CCD CAMERA" CHANNEL_ID = "CAM1" EXPOSURE_DURATION = 0.01 DATA_QUALITY_ID = "0" DATA_QUALITY_DESC = "0: Image Complete, 1: Lines Missing." INSTRUMENT_MODE_ID = "IMAGING" INSTRUMENT_MODE_DESC = "Instrument OPERATING MODE (from TM data)" INSTRUMENT_TEMPERATURE = ( -35.26 , -0.12 ) INSTRUMENT_TEMPERATURE_POINT = ( "CCD_T1", "OPTICS_T7" ) /*** ROSETTA MISSION SPECIFIC DATA DICTIONARY ENTRIES ***/ ROSETTA:CAM_ABSOLUTE_FRAME_NUMBER = 2323591 ROSETTA:CAM_MODE_FRAME_NUMBER = 844 ROSETTA:CAM_COVER_POSITION = FOC_NATT ROSETTA:CAM_GAIN = LOW ROSETTA:CAM_DATA_VALID = NOT_OK ROSETTA:CAM_WINDOW_POS_ALONG_ROW = 511 ROSETTA:CAM_WINDOW_POS_ALONG_COL = 511 ROSETTA:CAM_MISSING_LINES = 0 ROSETTA:PIPELINE_VERSION_ID = "1.1.3" /*** SPACECRAFT POSITION AND POINTING (J2000) ***/ COORDINATE_SYSTEM_ID = J2000 SC_SUN_POSITION_VECTOR = ( 418507553.597 , 5984700.149 , -41594098.327 ) SC_TARGET_POSITION_VECTOR = ( -7.105 , -1.153 , -71.865 ) SC_TARGET_VELOCITY_VECTOR = ( 0.124 , -0.280 , 0.045 ) TARGET_CENTER_DISTANCE = 72.225 SUB_SPACECRAFT_LATITUDE = 66.794247 SUB_SPACECRAFT_LONGITUDE = 118.015203 RIGHT_ASCENSION = 224.820570 DECLINATION = -86.190647 CELESTIAL_NORTH_CLOCK_ANGLE = 316.093556 SOLAR_ELONGATION = 87.072394 NOTE = "SPICE KERNELS USED: NAIF0011.TLS ROS_160517_STEP.TSC ROS_V26.TF RORB_DV_213_01_______00290.BSP RATT_DV_213_01_01____00290.BC CORB_DV_213_01_______00290.BSP CATT_DV_213_01_______00290.BC ROS_CHURYUMOV_V01.TF DE405.BSP The values of the keywords SC_SUN_POSITION_VECTOR, SC_TARGET_POSITION_VECTOR, SC_TARGET_VELOCITY_VECTOR, CELESTIAL_NORTH_CLOCK_ANGLE, RIGHT_ASCENSION, and DECLINATION are related to the equatorial J2000 inertial frame. The values of SUB_SPACECRAFT_LATITUDE and SUB_SPACECRAFT_LONGITUDE refer to the Cheops reference frame which is identical to the Flight Dynamics body-fixed frame implicitly specified by the information provided in the comet attitude file CATT. All values are computed for the time t = IMAGE_TIME. Distances are given in , velocities in , and angles in ." /*** IMAGE DESCRIPTION ***/ OBJECT = IMAGE DERIVED_MAXIMUM = 3602 DERIVED_MINIMUM = 176 LINES = 1024 LINE_SAMPLES = 1024 SAMPLE_TYPE = LSB_UNSIGNED_INTEGER SAMPLE_BITS = 16 SOURCE_SAMPLE_BITS = 12 SAMPLE_DISPLAY_DIRECTION = "RIGHT" LINE_DISPLAY_DIRECTION = "UP" END_OBJECT = IMAGE END