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/01/0013/01/00030/ 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 INT/ITZ/01/0016/01/00035/ 091295/180000000/ 35959.84572/88715.05648/22152.80699/ -.924155559/-1.35649809/-1.24150474/ 5913/ZZ INT/ITZ/01/0017/01/00038/ 201295/150000000/ 66193.97311/125081.0443/68021.87314/ -.493877253/-.426545715/-.879715685/ 5862/ZZ INT/ITZ/01/0018/01/00040/ 271295/170000000/ 81505.68772/133465.6068/99764.10893/ -.248422974/.0219077733/-.596556783/ 5892/ZZ