Format: F1 Orbital data as a state vectors, index : 1 Project: INT Satellite: ITP Synonimus: ITZ Launch date: 19950803 ----- TAIL PROBE, INTERBALL PROJECT ----- PROJ.launch: 19950803 Inertial coordinate system corresponds to equinox of equator of epoc: J2000 Situation calculation index : 2 Orbit calculation index: 3120300 GPC file name: gemt2.17 Harm. level : 4 Planets perturbation: ------------------------------------------------------------------------------ AAA INT/ITZ/01/0010/01/00021/ 171095/060000000/ 55734.37015/114070.6515/60193.50969/ -.616992495/-.661546315/-.989032276/ 5863/ZZ INT/ITZ/01/0011/01/00024/ 271095/070000000/ 88374.67865/120245.3074/127005.9760/ .0185611205/.3897256378/-.199616452/ 5879/ZZZ INT/ITZ/01/0012/01/00026/ 021195/160000000/ 55314.69454/42049.21975/99773.70012/ .7172391120/1.136329687/.9343622750/ 5877/ZZ INT/ITZ/01/0013/01/00030/ 191195/050000000/ 88139.78630/124348.3091/122994.4407/ -.024627609/.3298196548/-.290045584/ 5855/ZZ INT/ITZ/01/0014/01/00032/ 271195/100000000/ 80069.15629/132512.6356/98063.97524/ -.277747241/-.053608403/-.626586267/ 5857/ZZ INT/ITZ/01/0015/01/00034/ 021295/200000000/ 37053.70866/16623.87500/77117.92988/ 1.042010902/1.343765132/1.541050856/ 5817/ZZ