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/01/0118/02/00334/ 140199/200000001/ +038927.282/+027318.998/+069225.395/ +1.16182607/+1.96023604/+0.64572591/ ZZ INT/ITZ/01/0119/02/00341/ 100299/060000001/ +024884.738/+004562.449/+057421.729/ +1.54037599/+2.14273036/+1.36360158/ ZZ