LAUNCH INFORMATION
NAME: ARIANE 4 V137/TURKSAT-2A (EURASIASAT)
LAUNCH AGENCY: EUROPEAN SPACE AGENCY
LAUNCH SITE: GUIANA SPACE CENTER (CSG), PAD 2, F.G.
LAUNCH AZIMUTH: 083.0000 DEG
LAUNCH WINDOW: 08 JAN 01 2218Z TO 09 JAN 01 0026Z
LAUNCH VEHICLE: ARIANE 44 P
NOMINAL ORBITS
P/L SEP
EPOCH (D/HH:MM:SS.SSS): 008/22:38:20.803
PERIOD (MIN): 634.199
INCLINATION (DEG): 6.500
ECCENTRICITY (DEG): 0.731794
SEMI-MAJOR AXIS (KM): 24451.8033
ARGUMENT OF PERIGEE (DEG): 179.998
RA OF ASCENDING NODE (DEG): 261.187
MEAN ANOMALY (DEG): 1.639
START ORBIT TIME (HHH:MM:SS.SSS)MET:000:20:20.803
END ORBIT TIME (HHH:MM:SS.SSS)MET: 005:00:00.000
HEIGHT (KM): 241.3350
INJECTION LATITUDE (DEG): 1.57S
INJECTION LONGITUDE (DEG): 7.06E
INJECTION INERTIAL AZIMUTH (DEG): 96.288
INJECTION TIME (D/HH:MM:SS.SSS): 008/22:38:20.803
Keith Stein, Editor
Space & Missile Defense Report (SMDR)
http://www.kingpublishing.net
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This archive was generated by hypermail 2b29 : Mon Jan 08 2001 - 09:11:58 PST