
GeoLITE [NRO]
GeoLITE (Geosynchronous Lightweight Technology Experiment) was an advanced, experimental communications satellite featuring Laser and UHF communication devices. It is operated by the NRO.
GeoLITE was the first mission for TRW's T-310 satellite bus, a new lightweight, highly stable platform capable of a range of missions. TRW had system integration responsibility for GeoLITE, including the satellite development, integration and preparation for launch. Teammates included the Massachusetts Institute of Technology�s Lincoln Laboratory, which was responsible for the laser communications payload, and Hughes Space and Communications Company, which was responsible for the UHF communications payload
The laser communications experiments consisted of:
The UHF payload was part of the IBS-S (Integrated Broadcast Service - Simplex) inteligence data dissemination architecture to replace the older military satellite communications (MILSATCOM) archtecture. Other IBS-S payloads were flown on different missions to provide geostationary and polar coverage.
The satellite was designed and built in 3 1/2 years using streamlined program methodologies.
Note: The NROL designations refer to the launch, not to the payload.
| Nation: | USA |
|---|---|
| Type / Application: | Communication (Experimental) |
| Operator: | NRO |
| Contractors: | TRW (prime); Massachusetts Institute of Technology�s Lincoln Laboratory (laser payload); Hughes (IBS-S payload) |
| Equipment: | GLT, GLOM, IBS-S |
| Configuration: | T310 |
| Propulsion: | TR-500 SCAT |
| Power: | 2 deployable solar arrays, batteries |
| Lifetime: | 9 years |
| Mass: | ca. 1800 kg |
| Orbit: | GEO |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| GeoLITE (USA 158, NROL 17) | 2001-020A | 18.05.2001 | CC SLC-17B | Delta-7925 |