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/01/0133/01/00440/ 220200/090000001/ +084380.380/+170484.761/-003139.295/ -0.14894721/+0.18133226/-0.50432421/ 5836/ZZ INT/ITZ/01/0134/01/00452/ 090400/090000001/ +030510.578/+104380.680/-051116.228/ -0.77317406/-1.46641649/-0.05620441/ 5845/ZZ