Iridium Next SV155 - Norad Identifikationsnummer: 43573
| Name im Katalog Spacetrack | IRIDIUM 155 |
| Alternative Bezeichnung | Iridium Next SV155 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 155 | IRIDIUM 155 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 155 | Flugzeiten IRIDIUM 155 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 2999 |
| 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 155 | 789.86 km |
IRIDIUM 155 (also known as Iridium Next SV155) is a communication and traffic monitoring satellite launched on July 25, 2018, from AFWTR SLC4E using a Falcon 9 launch vehicle. The spacecraft has dimensions of 3.1 meters in length and 1.5 meters in diameter with a span of 9.4 meters. It features an ELiTeBus-1000 configuration and carries a L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and AIS-receiver (part of a set on 58 satellites). The satellite has a dry mass of 700 kg and a launch mass of 860 kg. It is powered by two deployable solar arrays and batteries. Designed for a lifetime of 10 years with plans for an extended operation up to 15 years, IRIDIUM 155 is owned by IRIDS and manufactured by NGISGA. The satellites shape is described as a half hex prism with two pans.
der Satellit IRIDIUM 155 hinausgetragen 25.07.2018r. Durchschnittshöhe IRIDIUM 155 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 155 beträgt 26856.99 km/h. Neigung IRIDIUM 155 Satelliten 86.4°.