
-


Object Name | DISCOVERER 36 |
---|---|
Object Full Name | - |
Norad ID | 213 |
Cospar ID | 1961-034A |
Object Type | Satellite |
Object Status | Decayed |
Object Class | - |
End of Life | - |
Discoverer 36 (1961 Alpha Kappa 1) was launched December 12, 1961, by the U.S. Air Force Space Systems Division into a polar orbit (perigee 148 miles, apogee 280 miles, inclination 81.2 deg) with a period of 91.5 min. The program objectives consisted of testing various space vehicle components, continuing evaluation of the Agena vehicle and recovery system, conducting experiments in radio propagation and radiation effects, and testing of instrumentation for nuclear explosion detection. The re-entry capsule was recovered from the ocean after four days and 64 orbits. The Discoverer 36 spacecraft re-entered March 8, 1962 (86 days after launch). The spacecraft weighed about 2100 lbs including 300 lb for the capsule, retrorocket, and recovery aids. Discoverer 36 carried, in addition to the capsule intended for recovery, a 10 lb piggyback satellite 'OSCAR' (Orbiting Satellite Carrying Amateur Radio) to beam signals to ham radio operators.
Launch Date | 1961-12-12 |
---|---|
Decay Date | 1962-03-08 |
Launch Vehicle | - |
Launch Site | Air Force Western Test Range, California, USA |
Launch Provider | - |
Launch Provider Country | - |
Launch Mass | - |
Dry Mass | - |
User | - |
---|---|
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 |
---|---|
Orbit | - |
Orbit Type | - |
Period: | 88.5 min |
Inclination: | 81.2° |
Apogee: | 207.0 km |
Perigee: | 194.0 km |
Longitude of Geo | - |
ECT | - |
Payload | - |
---|---|
Platform | - |
Propulsion | - |
Propulsion Type | - |
Life Time | - |
Power | - |
Budget | - |
Call Sign | - |
Beacon | - |
RCS | - |
References | - |
---|
Angular Momentum: | - |
---|---|
Eccentricity: | - |
Inclination: | - |
RAAN: | - |
Argument of Perigee: | - |
True Anomaly: | - |
Period: | - |
---|---|
Semi-Major Axis: | - |
Perigee: | - |
Apogee: | - |
Mean Motion: | - |
Mean Anomaly: | - |
Latitude: | - |
---|---|
Longitude: | - |
Altitude: | - |
Speed: | - |
Azimuth: | - |
Elevation: | - |
Range: | - |