Iridium Next SV125 - Norad Identifikationsnummer: 42964
| Name im Katalog Spacetrack | IRIDIUM 125 |
| Alternative Bezeichnung | Iridium Next SV125 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 125 | IRIDIUM 125 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 125 | Flugzeiten IRIDIUM 125 |
| In die Umlaufbahn bringen |
|
| 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 125 | 789.86 km |
The IRIDIUM 125 satellite, also known as Iridium Next SV125, was launched on October 9, 2017, from the AFWTR launch site using a Falcon 9 vehicle. It is owned by IRIDS and manufactured by OATKGA with a design lifetime of 10 years but planned for up to 15 years. The satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters, featuring the EliteBus configuration. It weighs 860 kg at launch and carries equipment including an L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver technology. Its purpose is communication and traffic monitoring, powered by two deployable solar arrays and batteries. The satellites shape is described as a half hex prism with two panels.
der Satellit IRIDIUM 125 hinausgetragen 09.10.2017r. Durchschnittshöhe IRIDIUM 125 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 125 beträgt 26856.99 km/h. Neigung IRIDIUM 125 Satelliten 86.4°.