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Object Name | MIDAS 5 (STRONGBACK) |
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Object Full Name | - |
Norad ID | 271 |
Cospar ID | 1962-010A |
Object Type | Satellite |
Object Status | - |
Object Class | - |
End of Life | - |
The MIDAS 5 (MIssile Defense Alarm System) satellite was designed primarily to detect the exhaust heat from a recently launched ICBM by use of infrared sensors. Secondary objectives included measuring cosmic radiation, energetic particles, and the effects of the space environment on certain metals and emulsions. The spacecraft was cylindrically shaped, measuring approximately 6 m in length and 1.5 m in diameter. Once in orbit, the spacecraft was stabilized in a nose-down attitude so that the IR sensors and antenna were always facing earthward.
Launch Date | 1962-04-09 |
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Decay Date | - |
Launch Vehicle | - |
Launch Site | Air Force Western Test Range, California, USA |
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 | United States |
Contractor | - |
Country of Contractor | - |
Payload Contractor | - |
Payload Contractor Country | - |
Orbit Status | Earth Orbit |
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Orbit | - |
Orbit Type | - |
Period: | 153.0 min |
Inclination: | 86.6° |
Apogee: | 3408.0 km |
Perigee: | 2786.0 km |
Longitude of Geo | - |
ECT | - |
Payload | - |
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Platform | - |
Propulsion | - |
Propulsion Type | - |
Life Time | - |
Power | - |
Budget | - |
Call Sign | - |
Beacon | - |
RCS | 8.2159 m² |
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: | - |