Iridium Next SV165 - Norad Identifikationsnummer: 43572
| Name im Katalog Spacetrack | IRIDIUM 165 |
| Alternative Bezeichnung | Iridium Next SV165 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 165 | IRIDIUM 165 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 165 | Flugzeiten IRIDIUM 165 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 2999 |
| 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) | 86.4° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 165 | 789.86 km |
IRIDIUM 165, also known as Iridium Next SV165, is a communication and traffic monitoring satellite operated by IRIDS (Iridium LLC). It was launched on July 25, 2018, from Vandenberg Air Force Base using a Falcon 9 launch vehicle. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters when its components are fully deployed. Its dry mass is 700 kg, and it has a launch mass of 860 kg. Equipped with an L-band payload for communication, Ka-band cross-links, downlinks, ADS-B payload, and an AIS-receiver (on 58 satellites), IRIDIUM 165 relies on two deployable solar arrays and batteries for power. The satellites configuration is based on the ELiTeBus-1000 bus manufactured by NGISGA and designed to have a lifetime of up to 10 years with plans for extended operations up to 15 years.
der Satellit IRIDIUM 165 hinausgetragen 25.07.2018r. Durchschnittshöhe IRIDIUM 165 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 165 beträgt 26856.98 km/h. Neigung IRIDIUM 165 Satelliten 86.4°.