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GEOStar-1
FURTHER INFORMATION ON THIS TOPIC AT OUR PARTNER SITE

?National Security satellite bus for use in ?GEO orbit and launch by ?Minotaur V, or Antares. Lifetime ?5-7 years and delivery possible ?27-30 months after receipt of order. Electrical system solar cells, average power 1.5kW

Status: In development 2016. Gross mass: 100 kg (220 lb).


More at: GEOStar-1.

Subtopics

Mitex American military anti-satellite system. 3 launched, 2006.06.21 (USA 187) to (USA 189). Technology satellite built by Orbital Sciences Corp. (OSC) for DARPA, USA. Launched 2006. Used the Aquila-Bus bus.

MITEx B Technology satellite built by Lockheed Martin for DARPA, USA. Launched 2006.

GSSAP Designed to catalog satellites and space debris in geostationary orbit. Built by Orbital for US Air Force Space Command. Orbit and mass classified; figures shown are speculative. Space surveillance satellite built by Orbital Sciences Corp. (OSC) for US Air Force, USA. Launched 2014 - 2016. Used the GeoStar-1 bus.

Bibliography: 12492.

2006 June 21 - . 22:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. Launch Pad: SLC17A. LV Family: Thor. Launch Vehicle: Delta 7925-9.5.
2014 July 28 - . 23:28 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC37B. Launch Pad: SLC37B. LV Family: Delta IV. Launch Vehicle: Delta 4M+(4,2).
2016 August 19 - . 04:52 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC37B. Launch Pad: Cape Canaveral SLC37B. LV Family: Delta IV. Launch Vehicle: Delta 4M+(4,2).

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