Zenit-2M

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Zenit-2M

Part of Zenit

Ukrainian orbital launch vehicle. Two-stage version of the Zenit-3SL booster developed for the Sea Launch program, modified for launch from ground facilities at Baikonur. Uses the common Zenit-2SB core vehicle with no upper stage.

AKA: Zenit-2SLB. Status: Active. First Launch: 2007-06-29. Last Launch: 2007-06-29. Number: 1 . Payload: 12,030 kg (26,520 lb). Thrust: 7,300.00 kN (1,641,100 lbf). Gross mass: 458,900 kg (1,011,700 lb). Height: 57.35 m (188.15 ft). Diameter: 3.90 m (12.70 ft). Apogee: 400 km (240 mi).

LEO Payload: 12,030 kg (26,520 lb) to a 400 km orbit at 51.60 degrees.

More at: Zenit-2M.

Family: orbital launch vehicle. Country: Ukraine. Spacecraft: Tselina-2. Launch Sites: Baikonur, Baikonur LC45/1. Stages: Zenit-A, Zenit-B. Agency: Yuzhnoye.

2007 June 29 - . 10:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-2M.

Cosmos 2428 - . Mass: 3,200 kg (7,000 lb). Nation: Russia. Agency: VKS. Manufacturer: Yuzhnoye. Class: Surveillance. Type: SIGINT. Spacecraft: Tselina-2. USAF Sat Cat: 31792 . COSPAR: 2007-029A. Apogee: 857 km (532 mi). Perigee: 846 km (525 mi). Inclination: 71.00 deg. Period: 102.00 min. Signals intelligence satellite. First launch in three years, and first with the improved version of the Zenit-2 launch vehicle using components developed for the Zenit-3SL..

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