GPS BIIF-4, GPS 2F-4, SVN 66, PRN 27, SLOT C2 - Norad ID: 39166
| Spacetrack Directory Name | NAVSTAR 68 (USA 242) |
| Alternative name | GPS BIIF-4, GPS 2F-4, SVN 66, PRN 27, SLOT C2 |
| Group | GPS |
| Follow NAVSTAR 68 (USA 242) | NAVSTAR 68 (USA 242) Tracker |
| Group follow GPS | Tracker GPS |
| Pass predictions NAVSTAR 68 (USA 242) | Pass predictions NAVSTAR 68 (USA 242) |
| Orbit launches |
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| Days in orbit | 4811 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Satellite |
| Categories | |
| Perigee | 19953 km |
| Apogee | 20411 km |
| Orbit slope (inclination) | 54.48° |
| Laps per day | 2 |
| Orbit | MEO (Non-Polar Inclined) |
| Height NAVSTAR 68 (USA 242) | 20191.85 km |
The NAVSTAR 68 (USA 242), also known as GPS IIF-4, is a navigation satellite operated by AFSMC and manufactured by BOES. It was launched on May 15, 2013, from SLC41 at AFETR using an Atlas V 401 launch vehicle. The satellite has dimensions of 2.5 meters in length and 1.8 meters in diameter with a span of 18 meters due to its solar arrays. It weighs 1630 kilograms at launch, with a dry mass of 1500 kilograms. Equipped with two deployable solar arrays and batteries for power supply, the satellite is configured as 3-Axis stabilized. Its mission, lasting 12 years, involves navigation purposes using its payload GPS SVN 66.
satellite NAVSTAR 68 (USA 242) Date of exalting 15.05.2013y. Average height of ISS NAVSTAR 68 (USA 242) hundred 20191.85 km. Average velocity NAVSTAR 68 (USA 242) is 13945.5 km/h. Inclination NAVSTAR 68 (USA 242) satellite 54.63°.