Iridium Next SV146 - Norad Identifikationsnummer: 43254
| Name im Katalog Spacetrack | IRIDIUM 146 |
| Alternative Bezeichnung | Iridium Next SV146 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 146 | IRIDIUM 146 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 146 | Flugzeiten IRIDIUM 146 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3117 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Typ | Satellit |
| Kategorie | |
| Perygeum | 776 km |
| Apogäum | 779 km |
| Neigung der Umlaufbahn (Inklination) | 86.39° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 146 | 789.86 km |
IRIDIUM 146, also known as Iridium Next SV146, is a communication and traffic monitoring satellite owned by IRIDS and launched on March 30, 2018, from AFWTR SLC4E using the Falcon 9 launch vehicle. It has a configuration of ELiTeBus-1000 with dimensions including a length of 3.1 meters, diameter of 1.5 meters, and span of 9.4 meters. The satellites dry mass is 700 kilograms and its launch mass was 860 kilograms. It carries L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and an AIS-receiver (part of a set on 58 satellites). Power is provided by two deployable solar arrays and batteries. Its shape is described as Half Hex Prism+2 pan, with a planned operational lifetime of up to 15 years beyond its designed lifespan of 10 years. The satellite was manufactured by OATKGA for communication purposes and traffic monitoring.
der Satellit IRIDIUM 146 hinausgetragen 30.03.2018r. Durchschnittshöhe IRIDIUM 146 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 146 beträgt 26856.99 km/h. Neigung IRIDIUM 146 Satelliten 86.4°.