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/01/0105/01/00276/ 090698/123000001/ 79443.70587/113028.5853/79296.70071/ .2614554286/.9205754534/-.460527825/ 5900/ZZ INT/ITZ/01/0106/01/00283/ 080798/123000001/ -10448.5745/14192.85316/-46445.5989/ -.917001146/-3.08507498/1.344719434/ 5897/ZZ INT/ITZ/01/0107/01/00289/ 280798/123000001/ 68829.80662/81084.22262/85177.68747/ .5212077826/1.292634796/-.169250515/ 5892/ZZ