Iridium Next SV127 - Norad Identifikationsnummer: 42956
| Name im Katalog Spacetrack | IRIDIUM 100 |
| Alternative Bezeichnung | Iridium Next SV127 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 100 | IRIDIUM 100 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 100 | Flugzeiten IRIDIUM 100 |
| In die Umlaufbahn bringen |
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| Tage im Orbit | 3288 |
| 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 100 | 789.86 km |
The IRIDIUM 100 (also known as Iridium Next SV127) satellite was launched on October 9, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle by owner IRIDS. It has a configuration of ELiTeBus-1000 and measures 3.1 meters in length with a diameter of 1.5 meters and a span of 9.4 meters. The satellites dry mass is 700 kg, and its launch mass was 860 kg. It is equipped with an L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver (on 58 satellites). Its power comes from two deployable solar arrays and batteries. The mission of IRIDIUM 100 is for communication and traffic monitoring purposes, designed to operate for 10 years with a planned lifetime extension to 15 years.
der Satellit IRIDIUM 100 hinausgetragen 09.10.2017r. Durchschnittshöhe IRIDIUM 100 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 100 beträgt 26856.99 km/h. Neigung IRIDIUM 100 Satelliten 86.4°.