; 070424AP_RE_90165_14363.bsp LOG FILE ; Created 2007-04-24/12:57:09.00. ; ; BEGIN SPKMERGE COMMANDS LEAPSECONDS_KERNEL = leapsecs SPK_KERNEL = 070424AP_RE_90165_14363.bsp SOURCE_SPK_KERNEL = sat267.bsp INCLUDE_COMMENTS = YES BODIES = 610, 611, 615, 616, 617 BEGIN_TIME = 1990 JUN 13 23:59:02.815 END_TIME = 2014 DEC 28 23:58:54.816 SOURCE_SPK_KERNEL = sat262.bsp INCLUDE_COMMENTS = YES BODIES = 612, 613, 614, 632 BEGIN_TIME = 1990 JUN 13 23:59:02.815 END_TIME = 2014 DEC 28 23:58:54.816 SOURCE_SPK_KERNEL = sat266.bsp INCLUDE_COMMENTS = YES BODIES = 618 BEGIN_TIME = 1990 JUN 13 23:59:02.815 END_TIME = 2014 DEC 28 23:58:54.816 SOURCE_SPK_KERNEL = sat268.bsp INCLUDE_COMMENTS = YES BODIES = 633 BEGIN_TIME = 1990 JUN 13 23:59:02.815 END_TIME = 2014 DEC 28 23:58:54.816 SOURCE_SPK_KERNEL = sat256.bsp INCLUDE_COMMENTS = YES BODIES = 634 BEGIN_TIME = 1990 JUN 13 23:59:02.815 END_TIME = 2014 DEC 28 23:58:54.816 SOURCE_SPK_KERNEL = sat265.bsp INCLUDE_COMMENTS = YES BODIES = 635 BEGIN_TIME = 1990 JUN 13 23:59:02.815 END_TIME = 2014 DEC 28 23:58:54.816 ; END SPKMERGE COMMANDS ; sat267.bsp LOG FILE ; ; Created 2007-04-24/09:51:33.00. ; ; BEGIN NIOSPK COMMANDS SPK_FILE = sat267.bsp INCLUDE_TEXT_FILE = delivery.sat267.txt SOURCE_NIO_FILE = /home/raj/Ephemerides/Saturn/sat267.nio BODIES = 610,611,615,616,617 BEGIN_TIME = CAL-ET 1990 JUN 14 00:00:00.000 END_TIME = CAL-ET 2014 DEC 29 00:00:00.000 ; END NIOSPK COMMANDS Filename: sat267.bsp Summary: Numerically integrated orbits for Janus, Epimetheus, Atlas, Prometheus, and Pandora fit to Earth-based, HST, Voyager, and Cassini data. Creator: Robert A. Jacobson Orbit Uncertainty for the years 2004-2009: Satellite R T N dl/dt (km) (km) (km) (deg/s) Janus 5 35 3 4.4e-09 Epimetheus 5 35 3 3.9e-09 Atlas 5 100 3 6.3e-09 Prometheus 5 50 3 4.3e-09 Pandora 5 50 3 1.1e-08 Epoch of the integration: JED 2453006.5 (02 January 2004) SPK Filename: sat267.bsp Usage, Restrictions, and Purpose: The use of this file is restricted to science planning (i.e., only for PDT design use within the SOP Implementation and SOP Update Processes), navigation, and impact avoidance activities until the file is placed in the PDS. Any proposed or intended scientific usage of this file or its contents before its placement in the PDS or publication by the Imaging Team, whichever comes first, must be discussed and accepted by the Imaging Team leader (as called for by the PSG-developed Cassini/Huygens Rules of the Road). ; sat262.bsp LOG FILE ; ; Created 2007-04-24/10:25:04.00. ; ; BEGIN NIOSPK COMMANDS SPK_FILE = sat262.bsp INCLUDE_TEXT_FILE = delivery.sat262.txt SOURCE_NIO_FILE = /home/raj/Ephemerides/Saturn/sat262xl.nio BODIES = 612,613,614,632 BEGIN_TIME = CAL-ET 1990 JUN 14 00:00:00.000 END_TIME = CAL-ET 2014 DEC 29 00:00:00.000 ; END NIOSPK COMMANDS Filename: sat262.bsp Summary: Numerically integrated orbits for Helene, Telesto, Calypso, and Methone fit to Earth-based, Voyager, HST, and Cassini data. These are from the SAT262 ephemeris which was fit to data through 15 April 2007. Body Identification: Code Name IAU designation 612 Helene SXII 613 Telesto SXIII 614 Calypso SXIV 632 Methone SXXXII (S/2004 S 1) Creator: Robert A. Jacobson Orbit Uncertainty: Satellite R T N dl/dt (km) (km) (km) (deg/s) Helene 5 25 5 1.2e-9 Telesto 5 25 5 1.7e-9 Calypso 5 25 5 1.7e-9 Methone 5 25 5 1.6e-9 Epoch of the integration: JED 2453582.5 (31-JUL-2005) SPK Filename: sat262.bsp Usage, Restrictions, and Purpose: The use of this file is restricted to science planning (i.e., only for PDT design use within the SOP Implementation and SOP Update Processes), navigation, and impact avoidance activities until the file is placed in the PDS. Any proposed or intended scientific usage of this file or its contents before its placement in the PDS or publication by the Imaging Team, whichever comes first, must be discussed and accepted by the Imaging Team leader (as called for by the PSG-developed Cassini/Huygens Rules of the Road). Filename: sat266.bsp Summary: Precessing ellipse orbit for Pan fit to Voyager data and Cassini imaging data; 86 Cassini images through 2007 February 6. Creator: Robert A. Jacobson Orbit Uncertainty: Satellite R T N dl/dt (km) (km) (km) (deg/s) Pan 3 10 3 4.6e-11 Epoch of the elements: Pan JED 2451545.0 SPK Filename: sat266.bsp Usage, Restrictions, and Purpose: The use of this file is restricted to science planning (i.e., only for PDT design use within the SOP Implementation and SOP Update Processes), navigation, and impact avoidance activities until the file is placed in the PDS. Any proposed or intended scientific usage of this file or its contents before its placement in the PDS or publication by the Imaging Team, whichever comes first, must be discussed and accepted by the Imaging Team leader (as called for by the PSG-developed Cassini/Huygens Rules of the Road). ; sat268.bsp LOG FILE ; ; Created 2007-04-24/12:56:07.00. ; ; BEGIN NIOSPK COMMANDS SPK_FILE = sat268.bsp INCLUDE_TEXT_FILE = delivery.sat268.txt SOURCE_NIO_FILE = /home/raj/Ephemerides/Saturn/sat268.nio BODIES = 633 BEGIN_TIME = CAL-ET 1990 JUN 14 00:00:00.000 END_TIME = CAL-ET 2014 DEC 29 00:00:00.000 ; END NIOSPK COMMANDS Filename: sat268.bsp Summary: Numerically integrated orbit for Pallene (S/2004 S 2). The orbit is fit to data from 128 Cassini images; the latest was on 07 February 2007. We also included the Voyager 2 observation of Pallene, originally identified as S/1981 S 14. Body Identification: Code Name IAU designation 633 Pallene SXXXIII (S/2004 S 2) Creator: Robert A. Jacobson Orbit Uncertainty: Satellite R T N dl/dt (km) (km) (km) (deg/s) Pallene 3 20 3 1.2e-09 Epoch of the integration: JED 2453060.5 (25 February 2004) SPK Filename: sat268.bsp Usage, Restrictions, and Purpose: The use of this file is restricted to science planning (i.e., only for PDT design use within the SOP Implementation and SOP Update Processes), navigation, and impact avoidance activities until the file is placed in the PDS. Any proposed or intended scientific usage of this file or its contents before its placement in the PDS or publication by the Imaging Team, whichever comes first, must be discussed and accepted by the Imaging Team leader (as called for by the PSG-developed Cassini/Huygens Rules of the Road). ; sat256.bsp LOG FILE ; ; Created 2006-09-27/12:56:02.00. ; ; BEGIN NIOSPK COMMANDS SPK_FILE = sat256.bsp INCLUDE_TEXT_FILE = delivery.sat256.txt SOURCE_NIO_FILE = /home/raj/Ephemerides/Saturn/sat256.nio BODIES = 634 BEGIN_TIME = CAL-ET 1990 JUN 14 00:00:00.000 END_TIME = CAL-ET 2014 DEC 29 00:00:00.000 ; END NIOSPK COMMANDS Filename: sat256.bsp Summary: Numerically integrated orbit for Polydeuces (S/2004 S 5) fit to Cassini data. The data arc extends from 2 April 2004 to 24 April 2006 and contains 155 observations. Creator: Robert A. Jacobson Body Identification: Code Name 634 Polydeuces Orbit Uncertainty: Satellite R T N dl/dt (km) (km) (km) (deg/s) Polydeuces 5 20 5 3.2e-9 Epoch of the integration: JED 2453006.50 (02-JAN-2004) SPK Filename: sat256.bsp Usage, Restrictions, and Purpose: The use of this file is restricted to science planning (i.e., only for PDT design use within the SOP Implementation and SOP Update Processes), navigation, and impact avoidance activities until the file is placed in the PDS. Any proposed or intended scientific usage of this file or its contents before its placement in the PDS or publication by the Imaging Team, whichever comes first, must be discussed and accepted by the Imaging Team leader (as called for by the PSG-developed Cassini/Huygens Rules of the Road). Filename: daphnis.bsp Summary: Precessing ellipse orbit for Daphnis fit to Cassini imaging data; 50 Cassini images through 2007 January 17. Body Identification: Code Name IAU designation 635 Daphnis S/2005 S 1 Creator: Robert A. Jacobson Orbit Uncertainty: Satellite R T N dl/dt (km) (km) (km) (deg/s) Daphnis 3 10 5 2.4e-10 Epoch of the elements: Daphnis JED 2453491.91412037 SPK Filename: daphnis.bsp Usage, Restrictions, and Purpose: The use of this file is restricted to science planning (i.e., only for PDT design use within the SOP Implementation and SOP Update Processes), navigation, and impact avoidance activities until the file is placed in the PDS. Any proposed or intended scientific usage of this file or its contents before its placement in the PDS or publication by the Imaging Team, whichever comes first, must be discussed and accepted by the Imaging Team leader (as called for by the PSG-developed Cassini/Huygens Rules of the Road).