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/01/0110/02/00304/                                                       
230998/123000001/                                                               
+073542.989/+093590.280/+081148.638/                                            
+0.43053927/+1.17621884/-0.29385340/                                            
ZZ                                                                              
INT/ITZ/01/0111/02/00310/                                                       
151098/123000001/                                                               
+011736.244/-013890.858/+049335.059/                                            
+1.68169250/+1.85148217/+2.24234405/                                            
ZZ