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/01/0099/01/00243/                                                       
040298/123000001/                                                               
83766.92324/124013.3406/79132.73091/                                            
.1082275319/.7192998691/-.553039774/                                            
5886/ZZ                                                                         
INT/ITZ/01/0100/01/00251/                                                       
060398/123000001/                                                               
76829.56147/97255.89656/91094.18064/                                            
.3422909244/1.041900058/-.314076887/                                            
5848/ZZ                                                                         
INT/ITZ/01/0101/02/00258/                                                       
010498/123000001/                                                               
+048361.818/+035970.946/+090206.901/                                            
+0.87835374/+1.57356972/+0.46335331/                                            
ZZ