MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "070305BP_SCPSE_07064_07073.xsp" PRODUCT_CREATION_TIME = 2007-03-05T12:33:30 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2007-03-05T12:26:56 STOP_TIME = 2007-03-14T13:49:00 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = { "CASSINI", "MERCURY BARYCENTER", "VENUS BARYCENTER", "EARTH BARYCENTER", "MARS BARYCENTER", "JUPITER BARYCENTER", "SATURN BARYCENTER", "URANUS BARYCENTER", "NEPTUNE BARYCENTER", "PLUTO BARYCENTER", "SUN", "MERCURY", "VENUS", "MOON", "EARTH", "MARS", "MIMAS", "ENCELADUS", "TETHYS", "DIONE", "RHEA", "TITAN", "HYPERION", "IAPETUS", "PHOEBE", "SATURN" } INSTRUMENT_NAME = "N/A" INSTRUMENT_ID = "N/A" SOURCE_PRODUCT_ID = "SEE COMMENTS" NOTE = "SPICE transfer format SPK file." ; bp_scpse.bsp LOG FILE ; ; Created 2007-03-05/12:33:24.00. ; ; BEGIN NIOSPK COMMANDS LEAPSECONDS_FILE = /cnav/inputs/naif/latest.tls SPK_FILE = bp_scpse.bsp INCLUDE_TEXT_FILE = spk_comments_bp_scpse.txt INCLUDE_TEXT_FILE = Readme SOURCE_NIO_FILE = /cnav/OD/deliveries/070305_040T26/p.nio BODIES = -82 BEGIN_TIME = CAL-ET 2007 MAR 05 12:28:01.000 END_TIME = CAL-ET 2007 MAR 14 13:50:05.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/070305_040T26/peph.nio BEGIN_TIME = CAL-ET 2007 MAR 05 12:28:01.000 END_TIME = CAL-ET 2007 MAR 14 13:50:05.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/070305_040T26/seph.nio BEGIN_TIME = CAL-ET 2007 MAR 05 12:28:01.000 END_TIME = CAL-ET 2007 MAR 14 13:50:05.000 ; END NIOSPK COMMANDS % template version $Revision: 1.13 $ $Date: 2006/08/18 20:07:20 $ - For OTM-097 based upon OD solution 070305_040T26. This file is invalid after 14-MAR-2007 13:50:05.0 ET or execution of subsequent maneuvers. This file does not include OTM-097 or its effects. Maneuvers prior to OTM-097 are included. This file includes planetary and satellite ephemerides. This file should only be used in case OTM-097 is NOT implemented. - FILENAME: 070305BP_SCPSE_07064_07073.BSP PURPOSE OF DELIVERY: OTM-097 (MAS ID O097_e) DELIVERY DATE: 070305 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 5-MAR-2007 12:28:01.0 ET SCET END EPOCH OF FILE: 14-MAR-2007 13:50:05.0 ET SCET ------ COMMENTS FROM NAV/MVR FOR OTM-097 O097_e By: Cassini-Huygens Navigation Team Profile file: MPF_O097_e_070305_040T26 Maneuver Start: 06-MAR-2007 23:06:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 070305_040T26 DELIVERY NAME: 070305_040T26 BY: Kevin Criddle DATE: March 05, 2007 PURPOSE OF DELIVERY: Final OD Delivery for OTM097 ORIGINAL DIRECTORY: /cnav/OD/ops/040T26/otm097/epoch_070211/070305 case 7 COMMENTS: Epoch of arc is 11-FEB-2007 12:00:00.000000000 Spacecraft a priori state and covariance from sat261 delivery Spacecraft State covariance with scale factor of 5 Satellite/planet Covariance sat261 2-way Doppler and Range through 05-MAR-2007 03:11 Optical Data through 26-FEB-2007 11:09 Weights by pass for F2 and SRA SMALL FORCES: SMFDV001 14-FEB-2007 06:49:31.6 SMFDV002 16-FEB-2007 07:56:46.3 SMFDV003 17-FEB-2007 06:04:49.7 SMFDV004 19-FEB-2007 08:34:02.4 SMFDV005 22-FEB-2007 02:31:08.0 SMFDV006 22-FEB-2007 03:48:16.6 SMFDV007 24-FEB-2007 05:43:16.3 SMFDV008 25-FEB-2007 08:27:39.5 SMFDV009 28-FEB-2007 06:10:02.8 SMFDV010 02-MAR-2007 06:17:15.3 SMFDV012 02-MAR-2007 09:06:01.1 MANEUVERS OTM094 19-FEB-2007 07:37 RCS burn w/ telem values OTM095 25-FEB-2007 Cancelled OTM096 02-MAR-2007 06:51 ME burn w/ telem values \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "070305BP_SCPSE_07064_07073.xsp" PRODUCT_CREATION_TIME = 2007-03-05T12:33:30 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2007-03-05T12:26:56 STOP_TIME = 2007-03-14T13:49:00 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = { "CASSINI", "MERCURY BARYCENTER", "VENUS BARYCENTER", "EARTH BARYCENTER", "MARS BARYCENTER", "JUPITER BARYCENTER", "SATURN BARYCENTER", "URANUS BARYCENTER", "NEPTUNE BARYCENTER", "PLUTO BARYCENTER", "SUN", "MERCURY", "VENUS", "MOON", "EARTH", "MARS", "MIMAS", "ENCELADUS", "TETHYS", "DIONE", "RHEA", "TITAN", "HYPERION", "IAPETUS", "PHOEBE", "SATURN" } INSTRUMENT_NAME = "N/A" INSTRUMENT_ID = "N/A" SOURCE_PRODUCT_ID = "SEE COMMENTS" NOTE = "SPICE transfer format SPK file." \endlabel Brief. Version: 2.2.0 (SPICE Toolkit N0058) Summary for: 070305BP_SCPSE_07064_07073.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- -82 CASSINI 2007 MAR 05 12:28:01.000 2007 MAR 14 13:50:05.000 1 MERCURY BARYCENTER Same coverage as previous object 2 VENUS BARYCENTER Same coverage as previous object 3 EARTH BARYCENTER Same coverage as previous object 4 MARS BARYCENTER Same coverage as previous object 5 JUPITER BARYCENTER Same coverage as previous object 6 SATURN BARYCENTER Same coverage as previous object 7 URANUS BARYCENTER Same coverage as previous object 8 NEPTUNE BARYCENTER Same coverage as previous object 9 PLUTO BARYCENTER Same coverage as previous object 10 SUN Same coverage as previous object 199 MERCURY Same coverage as previous object 299 VENUS Same coverage as previous object 301 MOON Same coverage as previous object 399 EARTH Same coverage as previous object 499 MARS Same coverage as previous object 601 MIMAS Same coverage as previous object 602 ENCELADUS Same coverage as previous object 603 TETHYS Same coverage as previous object 604 DIONE Same coverage as previous object 605 RHEA Same coverage as previous object 606 TITAN Same coverage as previous object 607 HYPERION Same coverage as previous object 608 IAPETUS Same coverage as previous object 609 PHOEBE Same coverage as previous object 699 SATURN Same coverage as previous object