Iridium Next SV134 - Norad Identifikationsnummer: 43075
| Name im Katalog Spacetrack | IRIDIUM 134 |
| Alternative Bezeichnung | Iridium Next SV134 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 134 | IRIDIUM 134 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 134 | Flugzeiten IRIDIUM 134 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3213 |
| 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 134 | 789.86 km |
IRIDIUM 134, also known as Iridium Next SV134, is a communication and traffic monitoring satellite manufactured by OATKGA for IRIDS (Iridium LLC). Launched on December 23, 2017, from the AFWTR SLC4E launch pad using a Falcon 9 rocket, this satellite has a BUS of EliteBus with the configuration ELiTeBus-1000. It measures 3.1 meters in length and 1.5 meters in diameter with a span of 9.4 meters. The dry mass is recorded at 700 kg while its launch mass was 860 kg. Equipped with deployable solar arrays and batteries for power, the satellite carries an L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver (part of a group of 58 satellites). The satellites design lifetime is ten years, with plans extending its operational life to fifteen years. Its shape is described as Half Hex Prism+2 pan.
der Satellit IRIDIUM 134 hinausgetragen 23.12.2017r. Durchschnittshöhe IRIDIUM 134 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 134 beträgt 26856.99 km/h. Neigung IRIDIUM 134 Satelliten 86.4°.