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/01/0108/01/00294/                                                       
170898/123000001/                                                               
82013.07922/150516.1024/36358.16061/                                            
-.161181521/.2761356682/-.754855171/                                            
5888/ZZ                                                                         
INT/ITZ/01/0109/01/00301/                                                       
120998/123000001/                                                               
82747.80285/125817.4203/67066.73045/                                            
.1520119749/.7892574010/-.559423175/                                            
5871/ZZ                                                                         
INT/ITZ/01/0110/01/00304/                                                       
230998/123000001/                                                               
+073542.989/+093590.280/+081148.638/                                            
+0.43053927/+1.17621884/-0.29385340/                                            
ZZ