Iridium Next SV143 - Norad Identifikationsnummer: 43258
| Name im Katalog Spacetrack | IRIDIUM 143 |
| Alternative Bezeichnung | Iridium Next SV143 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 143 | IRIDIUM 143 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 143 | Flugzeiten IRIDIUM 143 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3116 |
| 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) | 86.39° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 143 | 789.86 km |
The satellite IRIDIUM 143 (also known as Iridium Next SV143) was launched on March 30, 2018, from the Vandenberg Air Force Base using a Falcon 9 launch vehicle. It is part of a constellation owned by IRIDS and was manufactured by OATKGA. The satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters with its solar arrays deployed. Its dry mass is 700 kilograms and it had an initial launch mass of 860 kilograms. Equipped for communication and traffic monitoring purposes, it carries a L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver (shared across the constellation). The satellites power system consists of two deployable solar arrays and batteries to maintain its operations throughout its planned lifetime of 15 years. It has a configuration known as ELiTeBus-1000 and is part of the EliteBus bus series.
der Satellit IRIDIUM 143 hinausgetragen 30.03.2018r. Durchschnittshöhe IRIDIUM 143 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 143 beträgt 26856.99 km/h. Neigung IRIDIUM 143 Satelliten 86.4°.