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

---

Titan 401A/Centaur

---

AKA: Titan Centaur 401A. Status: Retired 1998. First Launch: 1994-02-07. Last Launch: 1998-08-12. Number: 9 . Thrust: 14,200.00 kN (3,192,200 lbf). Gross mass: 868,000 kg (1,913,000 lb). Height: 63.10 m (207.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 40,000 km (24,000 mi).

LEO Payload: 9,000 kg (19,800 lb). Payload: 9,000 kg (19,800 lb) to a GTO.

• USA 99 - . Payload: Milstar 1-01 / DFS 1. Mass: 4,500 kg (9,900 lb). Nation: USA. Agency: USAF. Class: Communications. Type: Military communications satellite. Spacecraft: Milstar. USAF Sat Cat: 22988 . COSPAR: 1994-009A. Apogee: 35,790 km (22,230 mi). Perigee: 35,733 km (22,203 mi). Inclination: 12.00 deg. Period: 1,434.00 min. Air Force Space Command launches the first Milstar satellite, a new generation military satellite communications system. Positioned in geosynchronous orbit at 90 deg W in 1994; 120 deg W in 1995-1999..

• USA 103 - . Payload: Raven 1. Mass: 5,200 kg (11,400 lb). Nation: USA. Agency: NRO, USAF. Class: Surveillance. Type: Naval signals intelligence satellite. Spacecraft: Raven satellite. USAF Sat Cat: 23097 . COSPAR: 1994-026A. Apogee: 537 km (333 mi). Perigee: 518 km (321 mi). Inclination: 55.10 deg. Period: 95.20 min. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

• USA 105 - . Payload: Mercury ELINT 1. Nation: USA. Agency: NRO, USAF. Class: Surveillance. Type: SIGINT. Spacecraft: Mercury ELINT. USAF Sat Cat: 23223 . COSPAR: 1994-054A. Apogee: 35,790 km (22,230 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. First launch of Mercury ELINT satellite..

• USA 110 - . Payload: Orion 3. Mass: 5,200 kg (11,400 lb). Nation: USA. Agency: CIA, NRO. Class: Surveillance. Type: SIGINT. Spacecraft: Advanced Orion. USAF Sat Cat: 23567 . COSPAR: 1995-022A. Apogee: 35,787 km (22,236 mi). Perigee: 35,787 km (22,236 mi). Inclination: 0.00 deg. Period: 1,440.00 min. First launch of 'Advanced Orion' (real code name unknown) new model geostationary ELINT satellite..

• USA 112 - . Payload: Raven 2. Mass: 5,200 kg (11,400 lb). Nation: USA. Agency: NRO, USAF. Class: Surveillance. Type: Naval signals intelligence satellite. Spacecraft: Raven satellite. USAF Sat Cat: 23609 . COSPAR: 1995-034A. Apogee: 39,000 km (24,000 mi). Perigee: 1,000 km (600 mi). Inclination: 64.00 deg. Period: 720.00 min.

• USA 115 - . Payload: Milstar DFS 2. Mass: 4,500 kg (9,900 lb). Nation: USA. Agency: USAF. Class: Communications. Type: Military communications satellite. Spacecraft: Milstar. USAF Sat Cat: 23712 . COSPAR: 1995-060A. Apogee: 35,787 km (22,236 mi). Perigee: 35,787 km (22,236 mi). Inclination: 10.00 deg. Secure military communication. Positioned in geosynchronous orbit at 4 deg E in 1995-2001. As of 2005 Mar 14 located at 10.26E drifting at 0.012E degrees per day..

• USA 118 - . Payload: Mercury ELINT 2. Nation: USA. Agency: NRO, USAF. Class: Surveillance. Type: SIGINT. Spacecraft: Mercury ELINT. USAF Sat Cat: 23855 . COSPAR: 1996-026A. Apogee: 35,790 km (22,230 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.00 min. Second launch of Mercury ELINT satellite..

• USA 136 - . Payload: Raven 3. Mass: 5,200 kg (11,400 lb). Nation: USA. Agency: NRO, USAF. Manufacturer: Kent. Class: Surveillance. Type: Naval signals intelligence satellite. Spacecraft: Raven satellite. USAF Sat Cat: 25034 . COSPAR: 1997-068A. Apogee: 39,059 km (24,270 mi). Perigee: 1,100 km (600 mi). Inclination: 63.60 deg. Period: 720.00 min.

• Mercury ELINT - . Payload: Mercury ELINT 3. Nation: USA. Agency: NRO, NSA. Manufacturer: TRW. Class: Surveillance. Type: SIGINT. Spacecraft: Mercury ELINT. Third launch of Mercury ELINT satellite..