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| Object Name | FLTSATCOM 8 (USA 46) |
|---|---|
| Object Full Name | - |
| Norad ID | 20253 |
| Cospar ID | 1989-077A |
| Object Type | Satellite |
| Object Status | Operational |
| Object Class | - |
| End of Life | - |
USA 46, a communications satellite also known as FLTSATCOM 8, was launched using the Atlas-Centaur launch vehicle from Cape Canaveral AFS. It was the last Atlas launch that NASA would manage; future unmanned NASA launches will be contracted from the private sector. FLTSATCOM provided worldwide UHF voice and teletype communications for US armed forces. It was specifically designed to communicate with small, inexpensive terminals used by field troops, and platforms aboard aircraft, ships and submarines. Twelve UHF channels were used by the Air Force, 10 by the Navy and one by the National Command Authority. An experimental EHF package aboard was a test bed for next-generation communications systems. Built by TRW Space and Technology Group, the 2,310-kg satellite's hexagonal body measured 2.46 m in diameter and 6.76 m high. It hosted an 18-turn helical UHF receive antenna and 4.9-m transmit antenna. Two 2.76 by 4 m solar panels and 3 nickel cadmium batteries provided 1,500 W of power over its 5-year service life. This satellite joined 5 operational satellites that had served the DoD since 1978.
| Launch Date | 1989-09-25 |
|---|---|
| Decay Date | - |
| Launch Vehicle | - |
| Launch Site | Air Force Eastern Test Range, Florida, USA |
| Launch Provider | - |
| Launch Provider Country | JM/2_09 |
| Launch Mass | - |
| Dry Mass | - |
| User | - |
|---|---|
| Mission | Communications |
| Mission Detail | - |
| Country of Registry | USA |
| Programme | - |
| Operator | US Navy |
| Country of Operator | United States |
| Contractor | Northrop Grumman (Former TRW) |
| Country of Contractor | USA |
| Payload Contractor | - |
| Payload Contractor Country | - |
| Orbit Status | Earth Orbit |
|---|---|
| Orbit | GEO |
| Orbit Type | -14,74 |
| Period: | 1436.2 min |
| Inclination: | 12.4° |
| Apogee: | 35814.0 km |
| Perigee: | 35761.0 km |
| Longitude of Geo | - |
| ECT | - |
| Payload | - |
|---|---|
| Platform | - |
| Propulsion | - |
| Propulsion Type | - |
| Life Time | - |
| Power | - |
| Budget | - |
| Call Sign | - |
| Beacon | - |
| RCS | 32.5418 m² |
| 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: | - |