Iridium Next SV106 - Norad Identifikationsnummer: 41917
| Name im Katalog Spacetrack | IRIDIUM 106 |
| Alternative Bezeichnung | Iridium Next SV106 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 106 | IRIDIUM 106 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 106 | Flugzeiten IRIDIUM 106 |
| 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 106 | 789.86 km |
IRIDIUM 106, also known as Iridium Next SV106, is a communication and traffic monitoring satellite operated by IRIDS (Iridium LLC). Launched on January 14, 2017, from AFWTR using a Falcon 9 launch vehicle from SLC4E, the satellite was manufactured by OATKGA. It measures 3.1 meters in length with a diameter of 1.5 meters and a span of 9.4 meters. The spacecraft has a dry mass of 700 kilograms and a launch mass of 860 kilograms. Equipped with L-band payload, Ka-band cross-links, and downlinks, it also carries ADS-B payload and AIS-receiver technology. Its power system includes two deployable solar arrays and batteries. Designed for a ten-year lifetime with plans for up to fifteen years, the satellites shape is described as a half hexagonal prism with two panels, having an RCS of 2.8038 square meters.
der Satellit IRIDIUM 106 hinausgetragen 14.01.2017r. Durchschnittshöhe IRIDIUM 106 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 106 beträgt 26856.99 km/h. Neigung IRIDIUM 106 Satelliten 86.4°.