Iridium Next SV162 - Norad Identifikationsnummer: 43482
| Name im Katalog Spacetrack | IRIDIUM 162 |
| Alternative Bezeichnung | Iridium Next SV162 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 162 | IRIDIUM 162 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 162 | Flugzeiten IRIDIUM 162 |
| In die Umlaufbahn bringen |
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| Tage im Orbit | 3063 |
| 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 | 746 km |
| Apogäum | 749 km |
| Neigung der Umlaufbahn (Inklination) | 86.45° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 162 | 759.88 km |
IRIDIUM 162 (also known as Iridium Next SV162) is a communication and traffic monitoring satellite owned by IRIDS and manufactured by OATKGA. Launched on May 22, 2018, from AFWTR SLC4E using the Falcon 9 launch vehicle, it has a configuration of ELiTeBus-1000 with dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. The satellites dry mass is 700 kg, with a launch mass of 860 kg. It is equipped with L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver (part of the equipment on 58 satellites). Its power comes from two deployable solar arrays and batteries. The satellites mission lifetime is designed for 10 years but planned to extend up to 15 years.
der Satellit IRIDIUM 162 hinausgetragen 22.05.2018r. Durchschnittshöhe IRIDIUM 162 Text Nummer 1: das. 759.88 km. Durchschnittsgeschwindigkeit IRIDIUM 162 beträgt 26913.34 km/h. Neigung IRIDIUM 162 Satelliten 86.45°.