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Object Name | COSMOS 49 |
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Object Full Name | - |
Norad ID | 913 |
Cospar ID | 1964-069A |
Object Type | Satellite |
Object Status | Decayed |
Object Class | - |
End of Life | - |
Cosmos 49 was instrumented with proton magnetometers to map the earth's magnetic field. This spacecraft, along with Cosmos 26, represented the U.S.S.R. contribution to the IQSY World Magnetic Survey. The corresponding U.S. measurements were performed on OGO 2 and OGO 4. The shape of the spacecraft was almost an ellipsoid and measured 1.8 m long and 1.2 m in diameter. A boom 3.3 m long was attached from one end of the spacecraft to the magnetometers. The performance of the spacecraft was satisfactory.
Launch Date | 1964-10-24 |
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Decay Date | 1965-08-21 |
Launch Vehicle | - |
Launch Site | Kapustin Yar Missile and Space Complex, Russia |
Launch Provider | - |
Launch Provider Country | - |
Launch Mass | - |
Dry Mass | - |
User | - |
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Mission | - |
Mission Detail | - |
Country of Registry | - |
Programme | - |
Operator | - |
Country of Operator | USSR/Russia |
Contractor | - |
Country of Contractor | - |
Payload Contractor | - |
Payload Contractor Country | - |
Orbit Status | Earth Orbit |
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Orbit | - |
Orbit Type | - |
Period: | 88.5 min |
Inclination: | 49.0° |
Apogee: | 212.0 km |
Perigee: | 186.0 km |
Longitude of Geo | - |
ECT | - |
Payload | - |
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Platform | - |
Propulsion | - |
Propulsion Type | - |
Life Time | - |
Power | - |
Budget | - |
Call Sign | - |
Beacon | - |
RCS | - |
References | - |
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Angular Momentum: | - |
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Eccentricity: | - |
Inclination: | - |
RAAN: | - |
Argument of Perigee: | - |
True Anomaly: | - |
Period: | - |
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Semi-Major Axis: | - |
Perigee: | - |
Apogee: | - |
Mean Motion: | - |
Mean Anomaly: | - |
Latitude: | - |
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Longitude: | - |
Altitude: | - |
Speed: | - |
Azimuth: | - |
Elevation: | - |
Range: | - |