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/01/0078/01/00168/                                                       
250497/100000000/                                                               
75827.84283/86650.42146/111399.1610/                                            
.3712947535/.9734349677/-.111250684/                                            
5870/ZZ                                                                         
INT/ITZ/01/0079/01/00175/                                                       
220597/100000000/                                                               
84311.54613/117368.9885/98633.85516/                                            
.1369415631/.6786527321/-.448250541/                                            
5891/ZZ