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ULAB

USA

Original archive entry. The text, images and links below are kept as they were written.

United Launch Alliance/Boeing

Country
USA

Chronology

1 event

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).
  • USA 253 - . Payload: GSSAP-1. Mass: 2,500 kg (5,500 lb). Nation: USA. Agency: ULAB. Spacecraft Bus: GeoStar-1. Spacecraft: GSSAP. USAF Sat Cat: 40099 . COSPAR: 2014-043A. Apogee: 35,500 km (22,000 mi). Perigee: 35,500 km (22,000 mi). Inclination: 0.00 deg. 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..
  • USA 254 - . Payload: GSSAP-2. Mass: 2,500 kg (5,500 lb). Nation: USA. Agency: ULAB. Spacecraft Bus: GeoStar-1. Spacecraft: GSSAP. USAF Sat Cat: 40100 . COSPAR: 2014-043B. Apogee: 35,500 km (22,000 mi). Perigee: 35,500 km (22,000 mi). Inclination: 0.00 deg. 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..
  • USA 255 - . Payload: ANGELS. Mass: 70 kg (154 lb). Nation: USA. Agency: ULAB. Spacecraft: ANGELS. USAF Sat Cat: 40101 . COSPAR: 2014-043C. Apogee: 35,500 km (22,000 mi). Perigee: 15,000 km (9,000 mi). Inclination: 25.00 deg.

    Small satellite for the Air Force Research Lab which made observations of the Delta rocket's second stage at ranges from 50 kilometers down to a few kilometers, for further development of satellite inspection technology. Orbit and mass classified; figures shown are speculative.