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/01/0130/01/00416/ 241199/090000001/ +053964.389/+143580.138/-043712.675/ -0.55555711/-0.79231008/-0.42674454/ 5886/ZZ INT/ITZ/01/0131/01/00422/ 151299/090000001/ +080191.953/+133375.098/+035175.016/ +0.26415836/+0.91265478/-0.46238956/ 5887/ZZ