Iridium Next SV172 - Norad Identifikationsnummer: 43927
| Name im Katalog Spacetrack | IRIDIUM 172 |
| Alternative Bezeichnung | Iridium Next SV172 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 172 | IRIDIUM 172 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 172 | Flugzeiten IRIDIUM 172 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 2829 |
| 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 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 172 | 789.86 km |
IRIDIUM 172, also known as Iridium Next SV172, is a communication and traffic monitoring satellite manufactured by NGISGA for IRIDS (Iridium). It was launched on January 11, 2019, from AFWTR SLC4E using the 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. Its configuration is ELiTeBus-1000 with a BUS type of EliteBus. It carries an L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and AIS-receiver among other equipment. The satellite has a dry mass of 700 kg and launch mass of 860 kg. Its power system includes two deployable solar arrays and batteries. The designed lifetime is 10 years with plans for a 15-year operation.
der Satellit IRIDIUM 172 hinausgetragen 11.01.2019r. Durchschnittshöhe IRIDIUM 172 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 172 beträgt 26856.99 km/h. Neigung IRIDIUM 172 Satelliten 86.4°.