NAVSTAR 64 (USA 206)

35752
Nummer im Katalog Spacetrack
2009-08-17
In die Umlaufbahn bringen
20190.51 km
Höhe Durchschnitt
13945.81 km/h
Durchschnittsgeschwindigkeit

Informationen über den Satelliten. NAVSTAR 64 (USA 206)

Name im Katalog Spacetrack NAVSTAR 64 (USA 206)
Alternative Bezeichnung GPS BIIRM-8, GPS 2R-21, SVN 50, PRN 05, SLOT E3
Gruppe GPS
Folge NAVSTAR 64 (USA 206) NAVSTAR 64 (USA 206) Tracker
Folge der Gruppe. GPS Tracker GPS
Flugzeiten NAVSTAR 64 (USA 206) Flugzeiten NAVSTAR 64 (USA 206)
In die Umlaufbahn bringen 2009-08-17 (15 vor Jahren)
Tage im Orbit 5764
Herkunftsland/-organisation USA (US)
Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. AFETR (Kennedy Space Center/Cape Canaveral, USA)
Kategorie
Perygeum 20028 km
Apogäum 20339 km
Neigung der Umlaufbahn (Inklination) 55.95°
Runden pro Tag 2
Orbit MEO (Nicht-polar geneigt)
Höhe NAVSTAR 64 (USA 206) 20190.51 km

Informationen über NAVSTAR 64 (USA 206)

USA-206, also GPS SVN-50, PRN-05 and NAVSTAR 64 and known before launch as GPS IIR-21, GPS IIRM-8 or GPS IIR-21(M), is an American navigation satellite which forms part of the Navstar Global Positioning System. It was the twenty-first and last Block IIR GPS satellite to be launched, and the eighth to use the modernised IIRM configuration.GPS IIR-21 was built by Lockheed Martin, based on the AS-4000 satellite bus, with the navigation payload being built by ITT. It was launched by a United Launch Alliance Delta II rocket, using the 7925-9.5 configuration, on 17 August 2009 at 10:35 GMT. It was the last spacecraft to launch from Space Launch Complex 17A at the Cape Canaveral Air Force Station, a launch pad which was first used in August 1957 for test flights of the PGM-17 Thor missile. It is also the final flight of an AS-4000 bus, the final GPS launch on a Delta II, and the final Delta II launch to be overseen by the US Air Force.Following separation from its carrier rocket, GPS IIR-21 received its USA designation, USA-206. It was deployed into a transfer orbit, from which raised itself to a semi-synchronous medium Earth orbit on 19 August, using an onboard Star 37FM apogee motor. It is a 2,032-kilogram (4,480 lb) satellite, and is expected to operate for at least ten years. Once it had completed on-orbit testing, it began covering Slot 3 of Plane E of the GPS constellation, replacing USA-126, or GPS IIA-26, which was launched in July 1996. It was declared operational on 27 August 2009.


== References ==

der Satellit NAVSTAR 64 (USA 206) hinausgetragen 17.08.2009r. Durchschnittshöhe NAVSTAR 64 (USA 206) Text Nummer 1: das. 20190.51 km. Durchschnittsgeschwindigkeit NAVSTAR 64 (USA 206) beträgt 13945.81 km/h. Neigung NAVSTAR 64 (USA 206) Satelliten 55.79°.

Orbital Elemente

Zeige formatiertes JSON.

Durchschnittshöhe der Orbitalbahn. NAVSTAR 64 (USA 206)

Durchschnittsgeschwindigkeit NAVSTAR 64 (USA 206)

Durchschnitt NAVSTAR 64 (USA 206)

Aktualisierungsdatum.: 2025-05-29 00:39:59
Durchschnittshöhe NAVSTAR 64 (USA 206) beträgt: 20190.51km
Durchschnittsgeschwindigkeit NAVSTAR 64 (USA 206) beträgt: 13945.81km/h
Durchschnittliche Neigung der Bahn NAVSTAR 64 (USA 206) beträgt: 55.79°
NAVSTAR 64 (USA 206) wurde am Tag in eine Umlaufbahn gebracht 2009-08-17
NAVSTAR 64 (USA 206) ist von 5764 Tage in der Umlaufbahn.