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Atlas V 411

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Status: Active. First Launch: 2006-04-20. Last Launch: 2018-01-20. Number: 5 . Payload: 8,763 kg (19,319 lb). Thrust: 5,188.00 kN (1,166,308 lbf). Gross mass: 386,800 kg (852,700 lb). Height: 59.10 m (193.80 ft). Diameter: 3.81 m (12.49 ft). Span: 5.36 m (17.58 ft).

• Astra 1KR - . Payload: A2100AXS. Mass: 4,332 kg (9,550 lb). Nation: Luxembourg. Agency: SES. Manufacturer: Lockheed. Program: Astra. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 29055 . COSPAR: 2006-012A. Apogee: 35,696 km (22,180 mi). Perigee: 35,631 km (22,140 mi). Inclination: 0.10 deg. Period: 1,429.80 min.

  The first Centaur upper stage burn placed the stack into a 167 km x 22442 km x 24.8 deg transfer orbit. After a second burn the Centaur released the satellite into a 6470 km x 36240 km x 23.8 deg orbit, from which it would use its own engine to achieve final geosynchronous orbit. As of 2007 Mar 10 located at 19.18E drifting at 0.022W degrees per day.

• USA 200 - . Payload: Raven 5 / NROL-28. Nation: USA. Agency: Martin. Class: Surveillance. Type: ELINT. Spacecraft: Raven satellite. USAF Sat Cat: 32706 . COSPAR: 2008-010A. Apogee: 35,780 km (22,230 mi). Perigee: 1,112 km (690 mi). Inclination: 63.60 deg. Period: 720.00 min.

  Classified National Reconnaisance Office satellite placed in a Molniya orbit; orbital parameters are estimated. Believed to be the second in a new series carrying combined signals intelligence and early warning payloads. Probable sensors included the SBIRS HEO-2 infrared missile early warning package and the NASA/Los Alamos TWINS-B magnetospheric research payload.

• USA 229 - . Payload: Intruder 9 / NROL-34. Mass: 3,250 kg (7,160 lb). Nation: USA. Class: Surveillance. Type: SIGINT. Spacecraft: Intruder. USAF Sat Cat: 37386 . COSPAR: 2011-014A. Apogee: 1,200 km (700 mi). Perigee: 1,010 km (620 mi). Inclination: 63.40 deg. Period: 107.40 min. Probable naval ocean surveillance satellite cluster; normally operate in 1100 km circular orbits with 63 deg inclination and carry equipment to track ships and aircraft via their radio transmissions..

• USA 229 P/L 2 - . Payload: Intruder 9 / NROL-34. Mass: 3,250 kg (7,160 lb). Nation: USA. Class: Surveillance. Type: SIGINT. Spacecraft: Intruder. USAF Sat Cat: 37391 . COSPAR: 2011-014B. Apogee: 1,200 km (700 mi). Perigee: 1,010 km (620 mi). Inclination: 63.40 deg. Period: 107.40 min. Probable naval ocean surveillance satellite cluster; normally operate in 1100 km circular orbits with 63 deg inclination and carry equipment to track ships and aircraft via their radio transmissions..

• OSIRIS-REx - . Nation: USA. Class: Astronomy. Type: Space probe. Spacecraft: OSIRIS-Rex. USAF Sat Cat: 41757 . COSPAR: 2016-055A. Apogee: -40,174 km (-40,174 mi). Perigee: 203 km (126 mi). Inclination: 29.50 deg.

  Asteroid sample return mission launched by a ULA Atlas V. The model 411 vehicle, serial AV-067, injected O-REx on a hyperbolic trajectory; the probe entered a 0.77 x 1.17 AU heliocentric orbit on Sep 12. OSIRIS-REx had a mass of 834 kg, and carried 1230 kg of propellant and a 46 kg sample return capsule identical to the one used by the Stardust mission. OSIRIS-REx was to make an Earth flyby in Sep 2017 to change its orbit to 0.90 x 1.35 AU x 6.4 deg, allowing it to rendezvous with asteroid (101955) Bennu in Aug 2018. The spacecraft was to sample the asteroid and return to Earth in 2023.

• SBIRS GEO-4 - . Payload: SBIRS GEO SV3; SBIRS GEO 4 (USA 282). Nation: USA. USAF Sat Cat: 43162 . COSPAR: 2018-009A. Apogee: 35,794 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 5.87 deg. Period: 1,436.10 min. See SBIRS-GEO 4 (USA 282). ..