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/01/0131/02/00422/ 151299/090000001/ +080197.677/+133339.318/+035165.986/ +0.26453697/+0.91294022/-0.46239368/ ZZ INT/ITZ/01/0132/02/00430/ 170100/090000001/ -005758.136/+021337.222/-038211.064/ -0.91251711/-3.25537445/+1.65548306/ ZZ INT/ITZ/01/0133/02/00440/ 220200/090000001/ +084393.018/+170477.317/-003071.237/ -0.14869739/+0.18172903/-0.50428710/ ZZ