Iridium Next SV169 - Norad Identifikationsnummer: 43926
| Name im Katalog Spacetrack | IRIDIUM 169 |
| Alternative Bezeichnung | Iridium Next SV169 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 169 | IRIDIUM 169 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 169 | Flugzeiten IRIDIUM 169 |
| 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 | 758 km |
| Apogäum | 768 km |
| Neigung der Umlaufbahn (Inklination) | 86.43° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 169 | 775.3 km |
IRIDIUM 169 (also known as Iridium Next SV169) is a communication and traffic monitoring satellite operated by IRIDS. It was launched on January 11, 2019, from the AFWTR Launch Site at SLC4E using a Falcon 9 launch vehicle. The satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. Its dry mass is 700 kg, with a launch mass of 860 kg. It is equipped with an L-band payload, Ka-band cross-links and downlinks, and an ADS-B payload (part of the configuration on 58 satellites). IRIDIUM 169s power comes from two deployable solar arrays and batteries. The satellites shape is described as a half hex prism with two panels, and it has been designed for a 10-year lifetime with plans for a 15-year operational span.
der Satellit IRIDIUM 169 hinausgetragen 11.01.2019r. Durchschnittshöhe IRIDIUM 169 Text Nummer 1: das. 775.3 km. Durchschnittsgeschwindigkeit IRIDIUM 169 beträgt 26884.32 km/h. Neigung IRIDIUM 169 Satelliten 86.42°.