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/01/0092/01/00214/ 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 INT/ITZ/01/0094/01/00220/ 111197/123000001/ -13054.4802/-27436.7707/-2676.49849/ .8451435534/-1.52921621/4.382385739/ 5848/ZZ INT/ITZ/01/0095/01/00223/ 201197/123000001/ 81955.85768/115446.2296/89455.70427/ .1885729008/.7907688889/-.468413691/ 5874/ZZ