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:           
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AAA                                                                             
INT/ITZ/01/0135/02/00463/                                                       
200500/090000001/                                                               
+069283.106/+163354.245/-034713.836/                                            
-0.40215485/-0.48570859/-0.36157887/                                            
ZZ                                                                              
INT/ITZ/01/0136/02/00470/                                                       
150600/090000001/                                                               
+083641.509/+175832.634/-016804.093/                                            
-0.18506918/-0.00835248/-0.40664303/                                            
ZZ                                                                              
INT/ITZ/01/0137/02/00477/                                                       
100700/090000001/                                                               
+057851.189/+080662.155/+030962.783/                                            
+0.83988310/+1.74772833/-0.16359141/                                            
ZZ