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/01/0088/01/00204/ 080997/210000000/ 68196.93392/68606.94709/105080.5740/ .5205493598/1.196006607/.0390036211/ 5907/ZZ INT/ITZ/01/0089/01/00208/ 260997/123000001/ 18615.25753/77077.12283/-38725.5708/ -1.05332366/-1.90520825/-.646305849/ 5898/ZZ INT/ITZ/01/0090/01/00212/ 091097/123000001/ 77574.45468/95014.02450/101256.7421/ .3303830880/.9785067811/-.259598694/ 5879/ZZ INT/ITZ/01/0091/01/00213/ 131097/123000001/ 82308.17410/110746.4679/95075.61472/ .2014051472/.8140559564/-.418685725/ 5865/ZZ INT/ITZ/01/0092/01/00214/ 171097/123000001/ 84866.16545/123960.0817/86449.69856/ .0878376384/.6446022873/-.551313150/ 5873/ZZ INT/ITZ/01/0093/01/00217/ 281097/123000001/ 77750.90918/97125.20386/99565.04375/ .3264699671/.9674953601/-.286557942/ 5912/ZZ