T310 (original) (raw)

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TRW satellite bus used for the 2000 GeoLite mission.

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	GeoLITE American military communications satellite. USA 158. GeoLITE was a TRW T-310 class satellite with a mass of about 1800 kg, including a solid apogee motor. Communication (Experimental) satellite built by TRW for NRO, USA. Launched 2001. Used the T310 bus.

SBIRS-Low-FDS 1, 2 Early warning satellite built by TRW for Missile Defense Agency (MDA) through the U.S. Air Force Space & Missile Systems Center (SMC),. Used the T310 bus.

2001 May 18 - . 17:45 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. Launch Pad: SLC17B. LV Family: Thor. Launch Vehicle: Delta 7925-9.5.

USA 158 - . Payload: GeoLITE. Mass: 93 kg (205 lb). Nation: USA. Agency: NRO. Manufacturer: TRW. Class: Communications. Type: Military communications satellite. Spacecraft Bus: T310. Spacecraft: GeoLITE. USAF Sat Cat: 26770 . COSPAR: 2001-020A. Apogee: 35,700 km (22,100 mi). Perigee: 179 km (111 mi). Inclination: 19.50 deg. Period: 629.01 min.
Military Communications Technology flight. Launch delayed from March 1, April 25, May 2 and 17. GeoLITE, US National Reconnaissance Office spacecraft was into placed by the Delta launch vehicle into a geostationary transfer orbit. GeoLITE was a TRW T-310 class satellite with a mass of about 1800 kg, including a solid apogee motor. The satellite carried an experimental laser communications payload and an operational UHF data relay payload.

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