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/01/0095/01/00223/                                                       
201197/123000001/                                                               
81955.85768/115446.2296/89455.70427/                                            
.1885729008/.7907688889/-.468413691/                                            
5874/ZZ                                                                         
INT/ITZ/01/0096/01/00230/                                                       
171297/123000001/                                                               
84338.23947/139255.7982/63993.55455/                                            
-.060067613/.4212147861/-.704725494/                                            
5851/ZZ                                                                         
INT/ITZ/01/0097/01/00232/                                                       
241297/123000001/                                                               
78635.00012/104681.7197/92566.13937/                                            
.2874445489/.9349308348/-.369613537/                                            
5877/ZZ