Iridium Next SV167 - Norad Identifikationsnummer: 43931
| Name im Katalog Spacetrack | IRIDIUM 167 |
| Alternative Bezeichnung | Iridium Next SV167 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 167 | IRIDIUM 167 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 167 | Flugzeiten IRIDIUM 167 |
| 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 167 | 789.86 km |
IRIDIUM 167, also known as Iridium Next SV167, is a communication and traffic monitoring satellite owned by IRIDS and manufactured by NGISGA. Launched on January 11, 2019, from AFWTR using the Falcon 9 launch vehicle, it has a configuration of ELiTeBus-1000 with dimensions: length 3.1 meters, diameter 1.5 meters, and span 9.4 meters. The satellites dry mass is 700 kg, while its launch mass was 860 kg. It is equipped with an L-band payload, Ka-band cross-links and downlinks, as well as ADS-B payload and AIS-receiver. Its power system includes two deployable solar arrays and batteries. Designed for a ten-year lifespan but planned for fifteen years of operation, the satellites shape is described as a half hex prism with two panels.
der Satellit IRIDIUM 167 hinausgetragen 11.01.2019r. Durchschnittshöhe IRIDIUM 167 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 167 beträgt 26856.98 km/h. Neigung IRIDIUM 167 Satelliten 86.4°.