Iridium Next SV137 - Norad Identifikationsnummer: 43076
| Name im Katalog Spacetrack | IRIDIUM 137 |
| Alternative Bezeichnung | Iridium Next SV137 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 137 | IRIDIUM 137 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 137 | Flugzeiten IRIDIUM 137 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3213 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Typ | Satellit |
| WWW | hier |
| Kategorie | |
| Perygeum | 776 km |
| Apogäum | 779 km |
| Neigung der Umlaufbahn (Inklination) | 86.39° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 137 | 789.86 km |
IRIDIUM 137, also known as Iridium Next SV137, is a communication and traffic monitoring satellite operated by IRIDS. It was launched on December 23, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. The spacecraft measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters when fully deployed. Weighing 860 kg at launch, its dry mass is 700 kg. It is equipped with L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and an AIS-receiver for traffic monitoring purposes. The satellites power source includes two deployable solar arrays and batteries. Its design aims for a 10-year operational lifetime with plans to extend up to 15 years. Manufactured by OATKGA, the satellite is part of the EliteBus configuration series.
der Satellit IRIDIUM 137 hinausgetragen 23.12.2017r. Durchschnittshöhe IRIDIUM 137 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 137 beträgt 26856.99 km/h. Neigung IRIDIUM 137 Satelliten 86.4°.