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Atlas E/OIS
Part of Atlas Family
American orbital launch vehicle. Atlas E + 1 x OIS upper stage.

Status: Retired 1985. First Launch: 1985-03-13. Last Launch: 1985-03-13. Number: 1 . Thrust: 1,731.00 kN (389,144 lbf). Gross mass: 120,000 kg (260,000 lb). Height: 28.70 m (94.10 ft). Diameter: 3.05 m (10.00 ft). Apogee: 800 km (490 mi).


More at: Atlas E/OIS.

Family: orbital launch vehicle. Country: USA. Spacecraft: Geosat. Launch Sites: Vandenberg, Vandenberg SLC3W. Stages: Atlas E/F, Atlas MA-3, Star 27. Agency: Convair.

1985 March 13 - . 02:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3W. LV Family: Atlas. Launch Vehicle: Atlas E/OIS.
  • Geosat - . Mass: 635 kg (1,399 lb). Nation: USA. Agency: USN. Class: Earth. Type: Earth resources radar satellite. Spacecraft: Geosat. USAF Sat Cat: 15595 . COSPAR: 1985-021A. Apogee: 779 km (484 mi). Perigee: 775 km (481 mi). Inclination: 108.1000 deg. Period: 100.40 min. Ocean sea height mapping. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C)..


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