Iridium Next SV124 - Norad Identifikationsnummer: 42810
| Name im Katalog Spacetrack | IRIDIUM 124 |
| Alternative Bezeichnung | Iridium Next SV124 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 124 | IRIDIUM 124 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 124 | Flugzeiten IRIDIUM 124 |
| 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 | 746 km |
| Apogäum | 749 km |
| Neigung der Umlaufbahn (Inklination) | 86.45° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 124 | 759.88 km |
IRIDIUM 124, also known as Iridium Next SV124, is a communication and traffic monitoring satellite operated by IRIDS (Iridium LLC). Launched on June 25, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle, the satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. It is equipped with an L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and AIS-receiver (on 58 satellites), and its configuration is based on the ELiTeBus-1000 bus manufactured by OATKGA. The satellite has a launch mass of 860 kg and a dry mass of 700 kg, powered by two deployable solar arrays and batteries. Its designed lifetime is 10 years with a planned extension to 15 years.
der Satellit IRIDIUM 124 hinausgetragen 25.06.2017r. Durchschnittshöhe IRIDIUM 124 Text Nummer 1: das. 759.88 km. Durchschnittsgeschwindigkeit IRIDIUM 124 beträgt 26913.34 km/h. Neigung IRIDIUM 124 Satelliten 86.45°.