Iridium Next SV131 - Norad Identifikationsnummer: 43079
| Name im Katalog Spacetrack | IRIDIUM 131 |
| Alternative Bezeichnung | Iridium Next SV131 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 131 | IRIDIUM 131 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 131 | Flugzeiten IRIDIUM 131 |
| 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 131 | 789.86 km |
IRIDIUM 131, also known as Iridium Next SV131, 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 satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters with its solar arrays deployed. It has a dry mass of 700 kg and a launch mass of 860 kg. Equipped with an L-band payload for communication, Ka-band cross-links and downlinks, as well as ADS-B and AIS-receivers (part of the configuration on 58 satellites), it was designed to have a lifetime of up to 15 years. The satellite is powered by two deployable solar arrays and batteries and has a half hex prism shape with two panels. It was manufactured by OATKGA as part of the EliteBus series, specifically the ELiTeBus-1000 configuration.
der Satellit IRIDIUM 131 hinausgetragen 23.12.2017r. Durchschnittshöhe IRIDIUM 131 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 131 beträgt 26856.99 km/h. Neigung IRIDIUM 131 Satelliten 86.4°.