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/01/0104/01/00270/                                                       
180598/123000001/                                                               
81363.60394/149167.3974/38061.41498/                                            
-.189546844/.1879528242/-.792646911/                                            
5910/ZZ                                                                         
INT/ITZ/01/0105/01/00276/                                                       
090698/123000001/                                                               
79443.70587/113028.5853/79296.70071/                                            
.2614554286/.9205754534/-.460527825/                                            
5900/ZZ