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/01/0068/01/00143/ 200197/140000000/ 77379.76712/88172.62085/113592.2210/ .3391670850/.9369926052/-.087630380/ 5905/ZZ INT/ITZ/01/0069/01/00145/ 280197/210000000/ 86323.90122/129947.0270/92325.57779/ -.044399576/.4399206245/-.568401169/ 5892/ZZ INT/ITZ/01/0070/01/00147/ 030297/180000000/ 9443.427696/-21610.7939/46947.50616/ 1.515596772/1.169277746/2.761946308/ 5872/ZZ INT/ITZ/01/0071/01/00149/ 120297/100000000/ 80092.96423/93282.30080/112616.4597/ .2893170491/.8921339139/-.154743966/ 5847/ZZ INT/ITZ/01/0072/01/00151/ 190297/180000000/ 71561.36191/70957.42006/112942.0414/ .4589428568/1.080461984/.0905129657/ 5906/ZZ INT/ITZ/01/0073/01/00154/ 030397/100000000/ 80576.92878/95570.21005/111606.6040/ .2749785540/.8753672585/-.188979191/ 5875/ZZ