Iridium Next SV109 - Norad Identifikationsnummer: 41919
| Name im Katalog Spacetrack | IRIDIUM 109 |
| Alternative Bezeichnung | Iridium Next SV109 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 109 | IRIDIUM 109 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 109 | Flugzeiten IRIDIUM 109 |
| 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 109 | 789.86 km |
The satellite IRIDIUM 109 (also known as Iridium Next SV109) was launched on January 14, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. It is owned by IRIDS and manufactured by OATKGA for communication and traffic monitoring purposes. The satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. Its dry mass is 700 kg with a launch mass of 860 kg. It features an L-band payload, Ka-band cross-links and downlinks, and ADS-B and AIS-receiver payloads (on 58 satellites). The satellites power source consists of two deployable solar arrays and batteries. Its design life is projected to be up to 15 years with a configuration known as ELiTeBus-1000.
der Satellit IRIDIUM 109 hinausgetragen 14.01.2017r. Durchschnittshöhe IRIDIUM 109 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 109 beträgt 26856.98 km/h. Neigung IRIDIUM 109 Satelliten 86.4°.