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/01/0132/02/00430/                                                       
170100/090000001/                                                               
-005758.136/+021337.222/-038211.064/                                            
-0.91251711/-3.25537445/+1.65548306/                                            
ZZ                                                                              
INT/ITZ/01/0133/02/00440/                                                       
220200/090000001/                                                               
+084393.018/+170477.317/-003071.237/                                            
-0.14869739/+0.18172903/-0.50428710/                                            
ZZ                                                                              
INT/ITZ/01/0134/02/00452/                                                       
090400/090000001/                                                               
+030411.466/+104228.759/-051162.094/                                            
-0.77387969/-1.46873727/-0.05451396/                                            
ZZ