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/01/0058/01/00127/ 211196/100000000/ 86998.62512/123912.6038/103726.0931/ .0322022476/.4941111961/-.469940446/ 5874/ZZ INT/ITZ/01/0059/01/00128/ 261196/100000000/ 58843.07058/124410.5766/23439.61734/ -.621359709/-.652844139/-1.01122354/ 5869/ZZ INT/ITZ/01/0060/01/00129/ 271196/080000000/ 170.8040925/-24664.9735/28966.93657/ 1.572912051/.5983699255/3.773661447/ 5904/ZZ INT/ITZ/01/0061/01/00130/ 031296/220000000/ 63125.77546/129115.4493/30607.20389/ -.559516287/-.519357581/-.981793054/ 5851/ZZ INT/ITZ/01/0062/01/00132/ 091296/140000000/ 68845.32750/68951.25414/115456.3635/ .4910535711/1.062317036/.1674634507/ 5886/ZZ INT/ITZ/01/0063/01/00135/ 201296/100000000/ 33903.35082/8163.488197/85359.83998/ 1.036436942/1.430720092/1.281659838/ 5870/ZZ INT/ITZ/01/0064/01/00136/ 241296/090000000/ 45761.99540/25857.46576/98397.51077/ .8488466666/1.360971297/.8312722984/ 5898/ZZ INT/ITZ/01/0065/01/00137/ 281296/020000000/ 39391.12759/14942.49631/91140.86216/ .9574410736/1.413342992/1.070830149/ 5892/ZZ