Iridium Next SV149 - Norad Identifikationsnummer: 43250
| Name im Katalog Spacetrack | IRIDIUM 149 |
| Alternative Bezeichnung | Iridium Next SV149 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 149 | IRIDIUM 149 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 149 | Flugzeiten IRIDIUM 149 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3116 |
| 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 149 | 789.86 km |
IRIDIUM 149, also known as Iridium Next SV149, is a communication and traffic monitoring satellite launched on March 30, 2018, from AFWTR SLC4E using a Falcon 9 launch vehicle. The spacecraft measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters when its solar arrays are deployed. It has a dry mass of 700 kilograms and was manufactured by OATKGA for IRIDS, the owner. Its primary equipment includes an L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver technology (present on 58 satellites). The satellite is powered by two deployable solar arrays and batteries and has a planned lifetime of up to 15 years. It operates in the shape of a Half Hex Prism with two panels and was designed for communication purposes as well as traffic monitoring.
der Satellit IRIDIUM 149 hinausgetragen 30.03.2018r. Durchschnittshöhe IRIDIUM 149 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 149 beträgt 26856.99 km/h. Neigung IRIDIUM 149 Satelliten 86.4°.