 | Resurs F-1
Credit - © Oliver Haßa
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Class: Earth. Type: Landsat. Destination: Surveillance Orbit. Nation: Russia. Agency: Russian Space Agency. Manufacturer: Kozlov. Variant of the Resurs-F recoverable earth resources satellite. See Resurs F1-17F40 for a full technical description. Typical orbit: 224 km circular orbit, 82.3 deg inclination. Mass: 6,300 kg (13,800 lb).
Resurs F1M Chronology - 1997 November 18 - Resurs F-1M - Program: Resurs. Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Perigee: 211 km (131 mi). Apogee: 238 km (147 mi). Inclination: 82.30 deg. Period: 89.00 min.
Landed in Kazakstan Dec 13.
- 1999 September 28 - Resurs F-1M - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Vehicle: Soyuz. Perigee: 220 km (130 mi). Apogee: 231 km (143 mi). Inclination: 82.30 deg. Duration: 24.00 days.
Remote sensing film satellite. Recovered in Russia on October 22, 1999.
Bibliography:- McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- McDowell, Jonathan, Jonathan's Space Report (Internet Newsletter), Harvard University, Weekly, 1989 to Present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- NASA GSFC Orbital Parameters,
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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