Iridium Next SV105 - Norad Identifikationsnummer: 41921
| Name im Katalog Spacetrack | IRIDIUM 105 |
| Alternative Bezeichnung | Iridium Next SV105 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 105 | IRIDIUM 105 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 105 | Flugzeiten IRIDIUM 105 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3556 |
| 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) | 86.4° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 105 | 789.7 km |
IRIDIUM 105 (also known as Iridium Next SV105) is a communication and traffic monitoring satellite manufactured by OATKGA for IRIDS (Iridium LLC). It was launched on January 14, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters. Equipped with L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and an AIS-receiver, the satellite has a dry mass of 700 kg and a launch mass of 860 kg. Its power source includes two deployable solar arrays and batteries. The satellite is designed for a lifespan of 10 years with plans to extend it up to 15 years.
der Satellit IRIDIUM 105 hinausgetragen 14.01.2017r. Durchschnittshöhe IRIDIUM 105 Text Nummer 1: das. 789.7 km. Durchschnittsgeschwindigkeit IRIDIUM 105 beträgt 26857.28 km/h. Neigung IRIDIUM 105 Satelliten 86.4°.