orbitparam.dat

   File_Format_Ver = 1.0
   Creation_Date = 2007-11-27T10:44:24.772
   ORIGINATOR    = HanDong

   Object_Name = CE-1
   Center_Name = MOON
   Reference_Frame = LCI
   Time_System = BJT

   Comment: State Vector.
   Epoch = 2007-12-03T09:00:00.000
   x  =    -162.0023715257091     [km]
   y  =    -1933.857171167550     [km]
   z  =     3.026611612663840     [km]
   vx =     0.04204810096698690   [km/s]
   vy =    -0.01232215819753885   [km/s]
   vz =     1.588354366841588     [km/s]

   Comment: Keplerian elements.
   Semi_major_axis   =     1932.652806175639     [km]
   Eccentricity      =    0.003606090476565559
   Inclination       =     88.45177560605939     [deg]
   Ra_of_asc_node    =     265.2090045338037     [deg]
   Arg_of_pericenter =     120.0                 [deg]
   Mean_anomaly      =     94.71685115019184     [deg]

   Comment: Parameters.
   Mass      =     1453.2340 [kg]
   Body_area =        3.440 [m**2]
   SA_area   =       26.784 [m**2]

   Comment: Perturbation information.
   PERT_ID   =      303
   NSP_M     =       64
   NSP_N     =       64
   SRP_CR    =        1.24
   DRG_CD    =        2.20
   DRG_KP    =        8.00
   DRG_F107  =      100.00
   DRG_F107P =      100.00