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/01/0025/01/00054/ 190296/150000000/ 49183.32004/111346.4847/39058.73895/ -.718298213/-.829537562/-1.07440360/ 5869/ZZ INT/ITZ/01/0026/01/00058/ 050396/100000000/ 68932.08908/129162.1421/69637.20826/ -.465660824/-.307569719/-.852232157/ 5904/ZZ INT/ITZ/01/0027/01/00060/ 130396/130000000/ 39917.10875/98440.87815/22808.00270/ -.859565282/-1.15974502/-1.17278877/ 5925/ZZ INT/ITZ/01/0028/01/00063/ 220396/140000000/ 75207.01070/74374.24368/122423.8265/ .4010896948/.8997422796/.2804587794/ 5846/ZZ INT/ITZ/01/0029/01/00065/ 010496/150000000/ 31513.41320/85477.17407/9387.679965/ -1.00184234/-1.52093000/-1.22851089/ 5872/ZZ