 | Okean-O1 Credit - © Mark Wade
| Other Designations: Sich-1. Class: Earth. Type: Radarsat. Destination: Medium Earth Orbit. Nation: Ukraine. Agency: RKA. Manufacturer: Yuzhnoye. Third generation Soviet oceanographic research satellite, equipped with a side-looking radar, radiometer, and multi-spectral scanner. Oceanographic research satellite, developed by KB-3 at NPO Yuzhnoye in the Ukraine, Vladimir Iosifovich Dranvoskiy, Chief Designer. The Okean oceanographic research satellite, later called Sich-1 by the Ukrainians, weighed 1950 kg, of which 505 kg was scientific instruments. Development was authorized on 5 May 1977 as one of the third generation of Soviet space systems. It was equipped with:
SUOS pointing, orientation, and stabilization system including:
Korall-A6 radio-command command-programming-trajectory system
BR-91Ts radiotelemetry system
STR thermoregulation system
SEP electrical feed system
SM-5 magnetometer
RFA radiophysical instrument with:
RLSBO side-looking radar with a swath width of 450 km and a resolution of 1.3 x 2.6 km
RM-0.8 scanning radiometer with a swath width of 550 km and a resolution of 25 km
RTBK radio-television complex with:
MSU-M 4-band multispectral scanner with a swath width of 1900 km and a resolution of 1.8 km
MSU-S 2-band multispectral scanner with a swath width of 1100 km and a resolution of 410 m
Kondor-2 system for interrogation, acquisition, storage, and dumping of data from Kondor-1 earth ground stations
Typical orbit: 631 km circular orbit, 82.5 deg inclination. Mass: 1,950 kg (4,290 lb). Associated Launch Vehicle: Tsyklon 3. Okean-O1 Chronology
- 1989 June 9 - Okean - Program: Okean. Launch Site: Plesetsk. Launch Vehicle: Tsyklon 3. FAILURE: Stage 3 failure - third stage engine did not ignite for second burn. Mass: 1,950 kg (4,290 lb).
- 1994 October 11 - Okean-O1 no. 7 - Program: Okean. Launch Site: Plesetsk. Launch Vehicle: Tsyklon 3. Mass: 1,950 kg (4,290 lb). Perigee: 631 km (392 mi). Apogee: 665 km (413 mi). Inclination: 82.54 deg. Period: 97.70 min.
Oceanography.
- 2004 December 24 - Sich-1M - Program: Okean. Launch Site: Plesetsk. Launch Vehicle: Tsyklon 3. FAILURE: Launch vehicle control system failure during third stage apogee kick burn. Mass: 2,263 kg (4,989 lb). Perigee: 280 km (170 mi). Apogee: 650 km (400 mi). Inclination: 82.56 deg.
Ukranian-built remote sensing satellite. Originally tagged by USAF SpaceCom as Cosmos 2412. Third stage apogee kick burn was too short, raising the perigee of the orbit from 78 km to 280 km, rather than the 650 km planned.
Bibliography and Further Reading
- McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
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