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Object Name | DISCOVERER 26 |
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Object Full Name | - |
Norad ID | 160 |
Cospar ID | 1961-016A |
Object Type | Satellite |
Object Status | Decayed |
Object Class | - |
End of Life | - |
Discoverer 26 was an earth-orbiting satellite designed to conduct scientific experiments, to test spacecraft engineering techniques, to evaluate the Agena B second-stage launch vehicle, and to attempt deceleration, reentry through the atmosphere, and recovery from the air of an instrument package. The 300-lb reentry capsule contained samples of silicon, iron, bismuth, yttrium, magnesium, nickel, lead, and uranium, which were exposed to the space environment for 50 hr 30 min. The payload also contained infrared sensors, photographic equipment, and other devices planned for use aboard the Midas and SAMOS satellites. The Agena B second stage contained instruments to measure the density and effects of ions and micrometeoroids at orbital altitude. This included an impact detector and a tuned piezoelectric crystal micrometeorite erosion gauge. The capsule successfully reentered the earth's atmosphere after 32 passes, and aerial recovery was accomplished. The Agena B stage remained in orbit and reentered the atmosphere December 5, 1961.
Launch Date | 1961-07-07 |
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Decay Date | 1961-12-05 |
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: | 89.0 min |
Inclination: | 82.9° |
Apogee: | 267.0 km |
Perigee: | 182.0 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: | - |