ULAB (original) (raw)
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
ULAB
United Launch Alliance/Boeing
Location: Denver-Centennial, Colorado.
Country: USA.
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.
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use