MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "060310BP_SCPSE_06069_06083.xsp" PRODUCT_CREATION_TIME = 2006-03-10T13:06:38 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2006-03-10T13:01:05 STOP_TIME = 2006-03-24T11:58:55 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 2006-03-10/13:06:32.00. ; ; 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/060310_022T12/p.nio BODIES = -82 BEGIN_TIME = CAL-ET 2006 MAR 10 13:02:10.000 END_TIME = CAL-ET 2006 MAR 24 12:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/060310_022T12/peph.nio BEGIN_TIME = CAL-ET 2006 MAR 10 13:02:10.000 END_TIME = CAL-ET 2006 MAR 24 12:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/060310_022T12/seph.nio BEGIN_TIME = CAL-ET 2006 MAR 10 13:02:10.000 END_TIME = CAL-ET 2006 MAR 24 12:00:00.000 ; END NIOSPK COMMANDS % template version $Revision: 1.11 $ $Date: 2005/11/15 15:49:49 $ - For OTM-055 based upon OD solution 060310_022T12. This file is invalid after 24-MAR-2006 12:00:00 UTC or execution of subsequent maneuvers. This file does not include OTM-055 or its effects. Maneuvers prior to OTM-055 are included. This file includes planetary and satellite ephemerides. This file should only be used in case OTM-055 is NOT implemented. - FILENAME: 060310BP_SCPSE_06069_06083.BSP PURPOSE OF DELIVERY: OTM-055 (MAS ID O055_g) DELIVERY DATE: 060310 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 10-MAR-2006 13:02:10.0 UTC SCET END EPOCH OF FILE: 24-MAR-2006 12:00:00 UTC SCET ------ COMMENTS FROM NAV/MVR FOR OTM-055 O055_g By: Cassini-Huygens Navigation Team Profile file: MPF_O055_g_060310_022T12 Maneuver Start: 16-MAR-2006 04:50:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 060310_022T12 -------------------------------------------------------------------------------- DELIVERY NAME: 060310_022T12 BY: Frederic J. Pelletier DATE: March 10, 2006 PURPOSE OF DELIVERY: Special OD delivery for live IVP Update ORIGINAL DIRECTORY: /cnav/OD/ops/022T12/otm055/epoch_060205/060310 case 8 COMMENTS: Epoch of arc is 05-FEB-2006 06:00:00 Spacecraft a priori state and covariance from sat240 delivery Spacecraft State covariance with scale factor of 5 Satellite/planet Covariance sat240 2-way Doppler and Range through 10-MAR-2006 09:26 Optical Data through 22-FEB-2006 11:43 Weights by pass for F2 and SRA 10-sec data used on T11 pass Titan J2,C22,S22 estimated 2.5 mm/s uncertainty used for all RCS burns Mass adjusted for OTM055 from MAS run Prediction for SMFDV357 (otm55 bias) using kpt pointing and fsds magnitude SMALL FORCES: SMFDV353 13-FEB-2006 07:28:14.0 SMFDV354 24-FEB-2006 07:38:50.5 SMFDV355 02-MAR-2006 06:50:57.3 SMFDV356 09-MAR-2006 05:22:08.1 MANEUVERS OTM053 - Mag, RA, Dec, ST ------------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "060310BP_SCPSE_06069_06083.xsp" PRODUCT_CREATION_TIME = 2006-03-10T13:06:38 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2006-03-10T13:01:05 STOP_TIME = 2006-03-24T11:58:55 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: 060310BP_SCPSE_06069_06083.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- -82 CASSINI 2006 MAR 10 13:02:10.000 2006 MAR 24 12:00:00.000 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