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Resurs F1M
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Resurs F-1
Credit: © Oliver Ha�a Russian earth land resources satellite. Variant of the Resurs-F recoverable earth resources satellite. See Resurs F1-17F40 for a full technical description. Earth Observation (film return) satellite built by TsSKB-Progress, Russia. Launched 1997 - 1999.
Status: Operational 1997. First Launch: 1997-11-18. Last Launch: 1999-09-28. Number: 2 . Gross mass: 6,300 kg (13,800 lb).
More at: Resurs F1M. Family: Earth, Earth land resource sat, Surveillance orbit. Country: Russia. Engines: 11D82M. Launch Vehicles: R-7, Soyuz-U, Soyuz-U-PVB. Projects: Resurs. Launch Sites: Plesetsk, Plesetsk LC43/4. Agency: Kozlov bureau. Bibliography: 2, 276, 4, 13015. Photo Gallery Resurs F-1M
Credit: Manufacturer Image 1997 November 18 - . 11:14 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
- Resurs F-1M - . Mass: 6,300 kg (13,800 lb). Nation: Russia. Agency: RAKA. Manufacturer: Kozlov bureau. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft Bus: Vostok. Spacecraft: Resurs F1M. Decay Date: 1997-12-13 . USAF Sat Cat: 25059 . COSPAR: 1997-072A. Apogee: 238 km (147 mi). Perigee: 211 km (131 mi). Inclination: 82.30 deg. Period: 89.00 min. Landed in Kazakstan Dec 13..
1999 September 28 - . 11:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. LV Family: R-7. Launch Vehicle: Soyuz-U-PVB.
- Resurs F-1M - . Mass: 6,300 kg (13,800 lb). Nation: Russia. Agency: RAKA. Manufacturer: Kozlov bureau. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft Bus: Vostok. Spacecraft: Resurs F1M. Duration: 24.00 days. Decay Date: 1999-10-22 . USAF Sat Cat: 25929 . COSPAR: 1999-054A. Apogee: 240 km (140 mi). Perigee: 214 km (132 mi). Inclination: 82.30 deg. Period: 89.00 min. Remote sensing film satellite. Recovered in Russia on October 22, 1999..
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