| Names | Navstar 5 GPS I-5 GPS SVN-5 |
|---|---|
| Mission type | Navigation Technology |
| Operator | US Air Force |
| COSPAR ID | 1980-011A[1] |
| SATCATno. | 11690 |
| Mission duration | 5 years (planned) 3.75 years (achieved) |
| Spacecraft properties | |
| Spacecraft | Navstar |
| Spacecraft type | GPS Block I |
| Manufacturer | Rockwell Space Systems[2] |
| Launch mass | 758 kg (1,671 lb) |
| Dimensions | 5.3 meters of long |
| Power | 400 watts |
| Start of mission | |
| Launch date | 9 February 1980, 23:08UTC |
| Rocket | Atlas F / SGS-1 (Atlas-35F) |
| Launch site | Vandenberg,SLC-3E |
| Contractor | Convair General Dynamics |
| Entered service | 27 February 1980 |
| End of mission | |
| Deactivated | 28 November 1983 |
| Orbital parameters | |
| Reference system | Geocentric orbit[3] |
| Regime | Medium Earth orbit (Semi-synchronous) |
| Perigee altitude | 20,144 km (12,517 mi) |
| Apogee altitude | 20,219 km (12,564 mi) |
| Inclination | 63.2° |
| Period | 717.94 minutes |
OPS 5117, also known asNavstar 5,GPS I-5 andGPS SVN-5, was an Americannavigation satellite launched in 1980 as part of theGlobal Positioning System development programme. It was the fifth of elevenBlock I GPS satellites to be launched.[2]
Global Positioning System (GPS) was developed by theU.S. Department of Defense to provide all-weather round-the-clock navigation capabilities for military ground, sea, and air forces. Since its implementation, GPS has also become an integral asset in numerous civilian applications and industries around the globe, including recreational used (e.g., boating, aircraft, hiking), corporate vehicle fleet tracking, and surveying. GPS employs 24 spacecraft in 20,200 km circular orbits inclined at 55°. These vehicles are placed in 6 orbit planes with four operational satellites in each plane.[1]
The first eleven spacecraft (GPS Block 1) were used to demonstrate the feasibility of the GPS system. They were 3-axis stabilized, nadir pointing usingreaction wheels. Dual solar arrays supplied over 400 watts. They hadS-band communications for control andtelemetry andUltra high frequency (UHF) cross-link between spacecraft. They were manufactured byRockwell Space Systems, were 5.3 meters across withsolar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block 1 spacecraft were inclined at 63°.[1]
OPS 5117 was launched at 23:08 UTC on 9 February 1980, atop anAtlas Flaunch vehicle with an SGS-1upper stage. The Atlas used had the serial number 35F, and was originally built as an Atlas F.[4] The launch took place fromSpace Launch Complex 3E atVandenberg Air Force Base,[5] and placed OPS 5117 into a transfer orbit. The satellite raised itself intomedium Earth orbit using aStar-27apogee motor.[2]
By 27 February 1980, OPS 5117 had been raised to an orbit with aperigee of 20,144 km (12,517 mi), anapogee of 20,219 km (12,564 mi), aperiod of 717.94 minutes, and 63.2° ofinclination to theequator.[6] The satellite had a design life of 5 years and a mass of 758 kg (1,671 lb).[2] It broadcast the PRN 05 signal in the GPS demonstration constellation, and was retired from service on 28 November 1983.
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