Iridium Next SV147 - Norad Identifikationsnummer: 43480
| Name im Katalog Spacetrack | IRIDIUM 147 |
| Alternative Bezeichnung | Iridium Next SV147 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 147 | IRIDIUM 147 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 147 | Flugzeiten IRIDIUM 147 |
| In die Umlaufbahn bringen |
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| Tage im Orbit | 3063 |
| 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) | 86.4° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 147 | 789.86 km |
IRIDIUM 147 (also known as Iridium Next SV147) is a communication and traffic monitoring satellite launched on May 22, 2018, from AFWTR SLC4E using a Falcon 9 launch vehicle. The satellite, with a configuration of ELiTeBus-1000 manufactured by OATKGA, measures 3.1 meters in length, 1.5 meters in diameter, and has a span of 9.4 meters. It was designed for a lifespan of 10 years but planned for 15 years of operation. Its dry mass is 700 kg, while its launch mass was 860 kg. The satellite is equipped with L-band payload, Ka-band cross-links and downlinks, as well as ADS-B and AIS-receiver payloads (the latter on 58 satellites). It operates using two deployable solar arrays and batteries for power. The satellites shape is described as a half hexagonal prism with two panels. Owned by IRIDS, it serves the mission of providing communication services and monitoring traffic.
der Satellit IRIDIUM 147 hinausgetragen 22.05.2018r. Durchschnittshöhe IRIDIUM 147 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 147 beträgt 26856.99 km/h. Neigung IRIDIUM 147 Satelliten 86.4°.