Ariane 4/ST-1 Elements

Keith Stein (kstein@launchspace.com)
Tue, 25 Aug 1998 14:09:09 -0700

ARIANE 4/ST-1 NOMINAL ORBITS
                                    ST-1 AT SEP                      
EPOCH (D/HH:MM:SS.SSS):             237/23:27:32.672                 
PERIOD (MIN):                       635.972                         
INCLINATION (DEG):                  4.000                          
ECCENTRICITY (DEG):                 0.728210                         
SEMI-MAJOR AXIS (KM):               24497.3326                       
ARGUMENT OF PERIGEE (DEG):          178.000                          
RA OF ASCENDING NODE (DEG):         149.605                          
MEAN ANOMALY (DEG):                 1.789                          
START ORBIT TIME (HHH:MM:SS.SSS)MET:000:20:32.672                    
END ORBIT TIME (HHH:MM:SS.SSS)MET:  016:00:00.000                    
HEIGHT (KM):                        365.2175                       
INJECTION LATITUDE (DEG):           0.99S                          
INJECTION LONGITUDE (DEG):          17.76E                          
INJECTION INERTIAL AZIMUTH (DEG):   93.930                          
INJECTION TIME (D/HH:MM:SS.SSS):    237/23:27:32.672


Keith Stein
Associate Technical Editor

Launchspace Publications, Inc.
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