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/01/0137/01/00477/ 100700/090000001/ +057823.783/+080589.234/+030912.807/ +0.84056096/+1.74913409/-0.16405467/ 5882/ZZ INT/ITZ/01/0138/01/00485/ 100800/090000001/ +085707.442/+147395.962/+011144.562/ +0.21508169/+0.77721309/-0.36896552/ 5881/ZZ