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/01/0098/01/00236/ 100198/123000001/ 41165.84531/115783.4494/-27204.0073/ -.775687727/-1.08081026/-.827981181/ 5890/ZZ INT/ITZ/01/0099/01/00243/ 040298/123000001/ 83766.92324/124013.3406/79132.73091/ .1082275319/.7192998691/-.553039774/ 5886/ZZ