Iridium Next SV176 - Norad Identifikationsnummer: 43923
| Name im Katalog Spacetrack | IRIDIUM 176 |
| Alternative Bezeichnung | Iridium Next SV176 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 176 | IRIDIUM 176 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 176 | Flugzeiten IRIDIUM 176 |
| 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 | 652 km |
| Apogäum | 656 km |
| Neigung der Umlaufbahn (Inklination) | 86.61° |
| Runden pro Tag | 15 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 176 | 666.11 km |
IRIDIUM 176, also known as Iridium Next SV176, is a communication and traffic monitoring satellite launched on January 11, 2019, from Vandenberg Air Force Base (AFWTR) using Falcon 9 as the launch vehicle. It was manufactured by NGISGA and owned by IRIDS. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and a span of 9.4 meters. It has a dry mass of 700 kg and a launch mass of 860 kg, featuring a configuration known as ELiTeBus-1000. Its equipment includes an L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver. The satellite is powered by two deployable solar arrays and batteries. It has a design lifetime of 10 years but plans are set for it to operate up to 15 years.
der Satellit IRIDIUM 176 hinausgetragen 11.01.2019r. Durchschnittshöhe IRIDIUM 176 Text Nummer 1: das. 666.11 km. Durchschnittsgeschwindigkeit IRIDIUM 176 beträgt 27091.91 km/h. Neigung IRIDIUM 176 Satelliten 86.61°.