GPS BIIF-10, GPS 2F-10, SVN 72, PRN 08, SLOT C3 - Norad Identifikationsnummer: 40730
| Name im Katalog Spacetrack | NAVSTAR 74 (USA 262) |
| Alternative Bezeichnung | GPS BIIF-10, GPS 2F-10, SVN 72, PRN 08, SLOT C3 |
| Gruppe | GPS |
| Folge NAVSTAR 74 (USA 262) | NAVSTAR 74 (USA 262) Tracker |
| Folge der Gruppe. GPS | Tracker GPS |
| Flugzeiten NAVSTAR 74 (USA 262) | Flugzeiten NAVSTAR 74 (USA 262) |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 4052 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Typ | Satellit |
| WWW | hier |
| Kategorie | |
| Perygeum | 20024 km |
| Apogäum | 20342 km |
| Neigung der Umlaufbahn (Inklination) | 53.94° |
| Runden pro Tag | 2 |
| Orbit | MEO (Nicht-polar geneigt) |
| Höhe NAVSTAR 74 (USA 262) | 20191.03 km |
NAVSTAR 74 (USA 262), also known as GPS IIF-10, is a US satellite designed for navigation purposes and was launched on July 15, 2015, from SLC41 at AFETR using an Atlas V 401 launch vehicle. The spacecraft has dimensions of 2.5 meters in length, 1.8 meters in diameter, and spans 18 meters with its solar arrays deployed. It weighs 1630 kg at launch and has a dry mass of 1500 kg. Equipped with 2 deployable solar arrays and batteries for power, it uses AOCS for motor control and is 3-Axis stabilized. The satellites purpose is navigation as part of the GPS system, carrying payload GPS SVN 72. It was manufactured by BOES for AFSMC and has a planned lifetime of 12 years.
der Satellit NAVSTAR 74 (USA 262) hinausgetragen 15.07.2015r. Durchschnittshöhe NAVSTAR 74 (USA 262) Text Nummer 1: das. 20191.03 km. Durchschnittsgeschwindigkeit NAVSTAR 74 (USA 262) beträgt 13945.7 km/h. Neigung NAVSTAR 74 (USA 262) Satelliten 54.08°.