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Apogee: 759 km (471 mi). Perigee: 526 km (326 mi). Inclination: 65.00 deg. Period: 97.60 min. Ocean monitoring.. 1981 March 20 - . 23:45 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. Launch Vehicle: Tsiklon-2. ...
Apogee: 759 km (471 mi). Perigee: 526 km (326 mi). Inclination: 65.00 deg. Period: 97.60 min. Ocean monitoring.. 1981 January 23 - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/1. LV Family: R-36. Launch Vehicle: Tsiklon-3. FAILURE: Payload shroud failed to separate.. ...
Apogee: 36,165 km (22,471 mi). Perigee: 35,902 km (22,308 mi). Inclination: 8.00 deg. Period: 1,448.70 min. Stationed at 140 deg E. Provision of telephone and telegraph radiocommunications and television broadcasting. Positioned in geosynchronous orbit at 140 deg E in 1989-1996 As ...
Perigee: 759 km (471 mi). Inclination: 98.40 deg. Period: 100.00 min. Soil Moisture and Ocean Salinity mission, obtaining climate-related data using a microwave aperture-synthesis interferometer.. PROBA-2 - . Mass: 130 kg (280 lb). Nation: Europe. Agency: KVR. Class: Technology. Type: ...
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Resurs-P went into a 190 km x 428 km initial orbit that was raised to its operational height of 330 km x 471 km on December 29. Sun synchronous orbit; 1150 GMT local time of the descending node.2015 June 23 - . 16:44 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43...
Perigee: 759 km (471 mi). Inclination: 98.40 deg. Period: 100.00 min. Soil Moisture and Ocean Salinity mission, obtaining climate-related data using a microwave aperture-synthesis interferometer.. 2010 October 19 - . 17:10 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV ...
AKA: K.Status: Cancelled 1965.Gross mass: 12,000 kg (26,000 lb). These would include highly maneuverable high performance storable liquid propellant engine modules; nuclear reactor modules for high power space applications; ion engine units for inter-orbital transfer and interplanetary flight; and...