Iridium Next SV141 - Norad Identifikationsnummer: 43077
| Name im Katalog Spacetrack | IRIDIUM 141 |
| Alternative Bezeichnung | Iridium Next SV141 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 141 | IRIDIUM 141 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 141 | Flugzeiten IRIDIUM 141 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3213 |
| 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) | 86.39° |
| Runden pro Tag | 14 |
| Höhe IRIDIUM 141 | 789.86 km |
IRIDIUM 141 (also known as Iridium Next SV141) is a communication and traffic monitoring satellite owned by IRIDS. Launched on December 23, 2017, from AFWTR SLC4E using the Falcon 9 launch vehicle, it has a dry mass of 700 kg and a launch mass of 860 kg. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and a span of 9.4 meters. It is equipped with an L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver technology. Its power system includes two deployable solar arrays and batteries. The design lifetime is planned for up to 15 years. Manufactured by OATKGA, the satellites shape is described as a half hex prism with two pans.
der Satellit IRIDIUM 141 hinausgetragen 23.12.2017r. Durchschnittshöhe IRIDIUM 141 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 141 beträgt 26856.99 km/h. Neigung IRIDIUM 141 Satelliten 86.4°.