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/01/0134/02/00452/ 090400/090000001/ +030411.466/+104228.759/-051162.094/ -0.77387969/-1.46873727/-0.05451396/ ZZ INT/ITZ/01/0135/02/00463/ 200500/090000001/ +069283.106/+163354.245/-034713.836/ -0.40215485/-0.48570859/-0.36157887/ ZZ INT/ITZ/01/0136/02/00470/ 150600/090000001/ +083641.509/+175832.634/-016804.093/ -0.18506918/-0.00835248/-0.40664303/ ZZ