Iridium Next SV180 - Norad Identifikationsnummer: 43922
| Name im Katalog Spacetrack | IRIDIUM 180 |
| Alternative Bezeichnung | Iridium Next SV180 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 180 | IRIDIUM 180 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 180 | Flugzeiten IRIDIUM 180 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 2829 |
| 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 180 | 789.86 km |
IRIDIUM 180 (also known as Iridium Next SV180) is a communication and traffic monitoring satellite manufactured by NGISGA for IRIDS. It was launched on January 11, 2019, from AFWTR SLC4E using the Falcon 9 launch vehicle. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and a span of 9.4 meters. Its dry mass is 700 kg and it has a launch mass of 860 kg. Equipped with L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver (on 58 satellites), IRIDIUM 180 features two deployable solar arrays and batteries for power generation. The satellite is designed to operate for up to 10 years but planned for a lifetime of 15 years. It has a shape described as Half Hex Prism+2 pan.
der Satellit IRIDIUM 180 hinausgetragen 11.01.2019r. Durchschnittshöhe IRIDIUM 180 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 180 beträgt 26856.99 km/h. Neigung IRIDIUM 180 Satelliten 86.4°.