NAVSTAR 65 (USA 213)
Satellite information NAVSTAR 65 (USA 213)
| Spacetrack Directory Name | NAVSTAR 65 (USA 213) |
| Alternative name | GPS BIIF-1, GPS 2F-1, SVN 62, PRN 25, SLOT B2 |
| Group | GPS |
| Follow NAVSTAR 65 (USA 213) | NAVSTAR 65 (USA 213) Tracker |
| Group follow GPS | Tracker GPS |
| Pass predictions NAVSTAR 65 (USA 213) | Pass predictions NAVSTAR 65 (USA 213) |
| Orbit launches |
2010-05-28 (16 years ago)
|
| Days in orbit | 5894 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Satellite |
| Categories | |
| Perigee | 19934 km |
| Apogee | 20431 km |
| Orbit slope (inclination) | 54.27° |
| Laps per day | 2 |
| Orbit | MEO (Non-Polar Inclined) |
| Height NAVSTAR 65 (USA 213) | 20191.7 km |
Additional information NAVSTAR 65 (USA 213)
NAVSTAR 65 (USA 213), also known as GPS IIF-1, is a navigation satellite launched by the United States Air Force Space and Missile Systems Center (AFSMC) on May 28, 2010, from Cape Canaveral Air Force Stations SLC37B pad using a Delta 4M+(4,2) launch vehicle. The spacecraft measures 2.5 meters in length with a diameter of 1.8 meters and spans 18 meters when its solar arrays are deployed. It has a dry mass of 1500 kg and was launched with a total mass of 1630 kg. This satellite is equipped with 2 deployable solar arrays and batteries for power supply, features a 3-axis stabilized configuration, and an AOCS (Attitude and Orbit Control System). Its mission is to provide navigation services as part of the GPS constellation, manufactured by Boeing (BOES) and designed with a lifespan of approximately 12 years.
satellite NAVSTAR 65 (USA 213) Date of exalting 28.05.2010y. Average height of ISS NAVSTAR 65 (USA 213) hundred 20191.7 km. Average velocity NAVSTAR 65 (USA 213) is 13945.53 km/h. Inclination NAVSTAR 65 (USA 213) satellite 54.3°.TLE
Average orbit height NAVSTAR 65 (USA 213)
Average velocity NAVSTAR 65 (USA 213)
Average inclination NAVSTAR 65 (USA 213)
ISS
Buy us a coffee!
