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/01/9002/01/00357/ 131299/130000001/ +082620.959/+158025.570/+019675.517/ -0.15372188/+0.23509137/-0.69542179/ 5895/ZZ INT/ITZ/01/9003/01/00367/ 210100/110000001/ +082659.807/+160052.532/+016212.927/ -0.13585270/+0.23166639/-0.67413773/ 5855/ZZ