Iridium Next SV123 - Norad Identifikationsnummer: 42804
| Name im Katalog Spacetrack | IRIDIUM 123 |
| Alternative Bezeichnung | Iridium Next SV123 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 123 | IRIDIUM 123 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 123 | Flugzeiten IRIDIUM 123 |
| 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 123 | 789.86 km |
IRIDIUM 123, also known as Iridium Next SV123, is a communication and traffic monitoring satellite operated by IRIDS. Launched on June 25, 2017, from Vandenberg Air Force Base (SLC4E) using the Falcon 9 launch vehicle, it was manufactured by OATKGA with a design lifetime of 10 years but planned for up to 15 years of operation. The satellite features a LENGTH of 3.1 meters, DIAMETER of 1.5 meters, and SPAN of 9.4 meters. It has a dry mass of 700 kg and was launched with a total mass of 860 kg. Equipped with L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and an AIS-receiver (on 58 satellites), IRIDIUM 123 utilizes two deployable solar arrays and batteries for power. Its shape is described as a Half Hex Prism+2 pan, without specific details on its color or RCS value.
der Satellit IRIDIUM 123 hinausgetragen 25.06.2017r. Durchschnittshöhe IRIDIUM 123 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 123 beträgt 26856.99 km/h. Neigung IRIDIUM 123 Satelliten 86.4°.