DAF/SPK NIO2SPK - %BIG-IEEE FTPSTR: : : : :::ENDFTP ; ap_scpse.bsp LOG FILE ; ; Created 2006-12-29/12:11:25.00. ; ; BEGIN NIOSPK COMMANDS LEAPSECONDS_FILE = /cnav/inputs/naif/latest.tls SPK_FILE = ap_scpse.bsp INCLUDE_TEXT_FILE = spk_comments_ap_scpse.txt INCLUDE_TEXT_FILE = Readme SOURCE_NIO_FILE = /cnav/Man/working/MAS/offline/prime/O086_g/p_with_mvr.nio BODIES = -82 BEGIN_TIME = CAL-ET 2006 DEC 27 00:00:00.000 END_TIME = CAL-ET 2007 JAN 17 20:39:36.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/061229_037T23/peph.nio BEGIN_TIME = CAL-ET 2006 DEC 27 00:00:00.000 END_TIME = CAL-ET 2007 JAN 17 20:39:36.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/061229_037T23/seph.nio BEGIN_TIME = CAL-ET 2006 DEC 27 00:00:00.000 END_TIME = CAL-ET 2007 JAN 17 20:39:36.000 ; END NIOSPK COMMANDS % template version $Revision: 1.14 $ $Date: 2006/08/18 20:07:29 $ - - For OTM-086 based upon OD solution 061229_037T23. This file is invalid after 17-JAN-2007 20:39 :36.0 ET or execution of subsequent maneuvers. This file accounts for maneuvers up to and including OTM-086. This file includes planetary and satellite ephemerides. - FILENAME: 061229AP_SCPSE_06361_07017.BSP PURPOSE OF DELIVERY: OTM-086 (MAS ID O086_g) DELIVERY DATE: 061229 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 27-DEC-2006 00:00:00 ET SCET END EPOCH OF FILE: 17-JAN-2007 20:39:36.0 ET SCET ------ COMMENTS FROM NAV/MVR FOR OTM-086 O086_g By: Cassini-Huygens Navigation Team Profile file: MPF_O086_g_061229_037T23 Maneuver Start: 31-DEC-2006 11:05:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 061229_037T23 -------------------------------------------------------------------------------- DELIVERY NAME: 061229_037T23 BY: Ruaraidh A. Mackenzie DATE: December 29, 2006 PURPOSE OF DELIVERY: Preliminary delivery for OTM086 ORIGINAL DIRECTORY: /cnav/OD/ops/037T23/otm086/ epoch_061222/061229 case 18 COMMENTS: Epoch of arc is 22-DEC-2006 06:00:00.000000000 Spacecraft a priori state and covariance from sat260 delivery Spacecraft State covariance with scale factor of 5 Satellite/planet Covariance sat260 2-way Doppler and Range through 29-DEC-2006 08:00 Optical Data through 17-DEC-2006 05:30 Weights by pass for F2 and SRA SMALL FORCES: SMFDV001 25-DEC-2006 12:37:07.5 SMFDV002 29-DEC-2006 04:53:47.5 MANEUVERS TBD ------------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "061229AP_SCPSE_06361_07017.xsp" PRODUCT_CREATION_TIME = 2006-12-29T12:11:42 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2006-12-26T23:58:55 STOP_TIME = 2007-01-17T20:38:31 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", "M IMAS", "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 @- @9 AG A: iAG A: i jAG A: j jAG A: j k|AG A: k} kAG A: k kAG A: k l0AG A: l1 l\AG A: l] lAG A: l lAG A: l m!AG A: - m" nDAG A: nE ogAG A: oh osAG A: + ot oAG A: o oAG A: Y o {AG A: Z { AG A: [ AG A: \ #AG A: ] $ UAG A: ^ V 9AG A: _ : AG A: ` aAG A: a b p_with_mvr.nio DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 DE-0414LE-0414 SATXXX SATXXX SATXXX SATXXX SATXXX SATXXX SATXXX SATXXX SATXXX a IAGX;k@h#tLb@x#tLb@I@#tLb@,Qz@I@"@RQ@oP@=@-z5 :@I/-@t 5BKl?xA`!hO,`҈A[_@>>EB=_A3=J