Iridium Next SV126 - Norad Identifikationsnummer: 42809
| Name im Katalog Spacetrack | IRIDIUM 126 |
| Alternative Bezeichnung | Iridium Next SV126 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 126 | IRIDIUM 126 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 126 | Flugzeiten IRIDIUM 126 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3394 |
| 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 126 | 789.86 km |
IRIDIUM 126, also known as Iridium Next SV126, is a communication and traffic monitoring satellite manufactured by OATKGA for IRIDS (Iridium). It was launched on June 25, 2017, from AFWTR using the Falcon 9 launch vehicle. The satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and a span of 9.4 meters. Its dry mass is 700 kilograms with a launch mass of 860 kilograms. Equipped with L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and an AIS-receiver (on 58 satellites), it operates on solar power using two deployable solar arrays and batteries. The satellites design lifetime is 10 years, but a planned extension could increase this to 15 years. Its shape is described as a half hex prism with two panels.
der Satellit IRIDIUM 126 hinausgetragen 25.06.2017r. Durchschnittshöhe IRIDIUM 126 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 126 beträgt 26856.98 km/h. Neigung IRIDIUM 126 Satelliten 86.4°.