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/01/0053/01/00119/ 231096/000000000/ 69550.50038/132865.3191/48255.25855/ -.469769699/-.324669843/-.924986630/ 5880/ZZ INT/ITZ/01/0054/01/00121/ 281096/130000000/ 56975.34464/44252.50705/109789.7177/ .6724354735/1.198469456/.5444781489/ 5888/ZZ INT/ITZ/01/0055/01/00123/ 051196/140000000/ 76534.01432/84212.62864/118843.8712/ .3631837128/.9136947516/.0000528588/ 5841/ZZ INT/ITZ/01/0056/01/00125/ 121196/080000000/ 25174.43872/-2513.91479/73947.67787/ 1.176998751/1.413035032/1.713396807/ 5898/ZZ INT/ITZ/01/0057/01/00125/ 151196/070000000/ 41797.59340/102980.2358/885.9344101/ -.859194671/-1.18766378/-1.07019957/ 5883/ZZ 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