; mar033_2000-2025.bsp LOG FILE
 
; Created 2001-08-19/14:24:56.00.
;
; BEGIN SPKMERGE COMMANDS
 
LEAPSECONDS_KERNEL   = /kernels/gen/lsk/naif0007.tls
 
SPK_KERNEL           = mar033_2000-2025.bsp
  SOURCE_SPK_KERNEL  = mar033-7.bsp
    INCLUDE_COMMENTS = NO
    BODIES           = 10, 399, 3, 4, 499, 402, 401
    BEGIN_TIME       = 2000 JAN 01 00:00:00.000
    END_TIME         = 2025 JAN 01 00:00:00.000
 
; END SPKMERGE COMMANDS
 
The file mar033_2000-2025.bsp was created on August 19, 2001, using
the SPICE utility SPKMERGE to crerate a subset of the file
mar033-7.bsp covering only the period of 2000 JAN 01 to 2025 JAN 01.
 
 
The summary of this file, made using the SPICE utility BRIEF is as follows:
 
Summary for: mar033_2000-2025.bsp
 
Bodies: EARTH BARYCENTER (3) w.r.t. SOLAR SYSTEM BARYCENTER (0)
        MARS BARYCENTER (4) w.r.t. SOLAR SYSTEM BARYCENTER (0)
        SUN (10) w.r.t. SOLAR SYSTEM BARYCENTER (0)
        EARTH (399) w.r.t. EARTH BARYCENTER (3)
        PHOBOS (401) w.r.t. MARS BARYCENTER (4)
        DEIMOS (402) w.r.t. MARS BARYCENTER (4)
        MARS (499) w.r.t. MARS BARYCENTER (4)
        Start of Interval (ET)              End of Interval (ET)
        --------------------------------    --------------------------------
        2000 JAN 01 00:01:04.183            2025 JAN 01 00:01:04.183
 
 
The file release form for the source file, named mar033.7, is included below for
reference purposes.
 
 
Satellite Ephemeris: MAR033.7
 
File location: murphy:/home5/raj/Ephemerides/Mars/mar033.7.nio
 
Enter SATGEN/7  2-MAR-1998 10:30:30 linked 19-JUN-1997 11:48:08
Sinclair/Morley theory fit to data - GMM-1 gravity field
Ephemeris Version Number:  7
Timespan from JED  2442930.500(01-JUN-1976) to JED  2460687.500(12-JAN-2025)
File Epoch Julian Date: 2433282.50
Master Interval =    9.0000 Days
Equinox Reference Julian Date: 2451545.00
Planetary Ephemeris Number: DE400  /LE400
 
Bodies on the File:
 
    Name          Number          GM                NDIV   NDEG   Model
 
    Phobos         401     6.900000000000000E-04     21     15    MARROG
    Deimos         402     1.200000000000000E-04      4     15    MARROG
    Mars           499     4.282831000000000E+04      1      2    MARROG
    System                 4.282831081000000E+04
 
Additional Constants on the File:
 
    AU       1.495978706930000E+08   RADIUS   3.394200000000000E+03
    J402     1.958744236927738E-03   J404    -1.544758500000000E-05
    J406    -4.809812929590655E-06   POLTIM   2.451545000000000E+06
    ZACPL4   3.176810000000000E+02   ZDEPL4   5.288600000000000E+01
    DACPL4  -1.082634477472879E-01   DDEPL4  -6.145938682503714E-02
    WPL4     1.768680000000000E+02   WDP4     3.508919830000000E+02
    J403     3.150092540660739E-05   J405     5.848879915442181E-06
    J407    -5.044821990079402E-06   J408    -4.436044287664986E-07
    C40201   4.800265282192135E-09   S40201   8.433782202002733E-09
    C40202  -5.442562507653622E-05   S40202   3.207439707968164E-05
    C40301   4.149159315808776E-06   S40301   2.730396370566899E-05
    C40302  -5.438445464054723E-06   S40302   2.880981952778337E-06
    C40303   4.938440449888407E-06   S40303   3.508686713137301E-06
    C40401   4.055607395939038E-06   S40401   3.503672289945575E-06
    C40402  -2.507508521175496E-07   S40402  -2.005652604558221E-06
    C40403   3.867691075800419E-07   S40403  -1.464301447639094E-08
    C40404   2.243073658508141E-09   S40404  -2.716835353360919E-07
 
Ephemeris Accuracy (km,sec) - 1 sigma:
 
    Name               Radial    Downtrack       Normal       Period
    Phobos              3.000       15.000        7.000     0.000100
    Deimos              3.000       30.000       16.000     0.000400
 
 
Chebyshev interpolation error:  50.00 meters
 
Release to: Mars Projects                      Time: 16-MAR-1998 08:52:01
 
Preparer: R.A.  Jacobson
 
Comments:
Extended ephemeris for mission studies.  Orbital motion model is the extended
Sinclair/Morley theory fit to astrometric and spacecraft observations.  File
contains 39196672 bytes.