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/01/9001/01/00351/                                                       
221199/150000001/                                                               
+056624.004/+144662.350/-030556.334/                                            
-0.55907147/-0.63669993/-0.66166040/                                            
5875/ZZ                                                                         
INT/ITZ/01/9002/01/00357/                                                       
131299/130000001/                                                               
+082620.959/+158025.570/+019675.517/                                            
-0.15372188/+0.23509137/-0.69542179/                                            
5895/ZZ