Iridium Next SV139 - Norad Identifikationsnummer: 42963
| Name im Katalog Spacetrack | IRIDIUM 139 |
| Alternative Bezeichnung | Iridium Next SV139 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 139 | IRIDIUM 139 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 139 | Flugzeiten IRIDIUM 139 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3288 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Typ | Satellit |
| WWW | hier |
| Kategorie | |
| Perygeum | 776 km |
| Apogäum | 779 km |
| Neigung der Umlaufbahn (Inklination) | 86.4° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 139 | 789.86 km |
IRIDIUM 139, also known as Iridium Next SV139, is a communication and traffic monitoring satellite built by OATKGA for IRIDS (Iridium LLC). Launched on October 9, 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 a span of 9.4 meters. It features an EliteBus configuration with a dry mass of 700 kg and was designed for a 10-year lifetime but planned for up to 15 years. Equipped with L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver, the satellite is powered by two deployable solar arrays and batteries. Its shape is described as Half Hex Prism+2 pan.
der Satellit IRIDIUM 139 hinausgetragen 09.10.2017r. Durchschnittshöhe IRIDIUM 139 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 139 beträgt 26856.99 km/h. Neigung IRIDIUM 139 Satelliten 86.4°.