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/01/0103/01/00262/ 160498/123000001/ 33106.89919/11543.96293/79181.80502/ 1.139417593/1.732380485/1.011728263/ 5875/ZZ INT/ITZ/01/0104/01/00270/ 180598/123000001/ 81363.60394/149167.3974/38061.41498/ -.189546844/.1879528242/-.792646911/ 5910/ZZ