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/01/0097/01/00232/ 241297/123000001/ 78635.00012/104681.7197/92566.13937/ .2874445489/.9349308348/-.369613537/ 5877/ZZ INT/ITZ/01/0098/01/00236/ 100198/123000001/ 41165.84531/115783.4494/-27204.0073/ -.775687727/-1.08081026/-.827981181/ 5890/ZZ