Iridium Next SV158 - Norad Identifikationsnummer: 43571
| Name im Katalog Spacetrack | IRIDIUM 158 |
| Alternative Bezeichnung | Iridium Next SV158 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 158 | IRIDIUM 158 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 158 | Flugzeiten IRIDIUM 158 |
| 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 158 | 789.86 km |
IRIDIUM 158 (also known as Iridium Next SV158) is a communication and traffic monitoring satellite operated by IRIDS. It was launched on July 25, 2018, from AFWTR SLC4E using a Falcon 9 launch vehicle. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters when its solar arrays are deployed. Its dry mass is 700 kg, and it was launched with a total mass of 860 kg. Equipped with an L-band payload for communication, Ka-band cross-links, and downlinks, as well as ADS-B and AIS-receiver capabilities (shared among 58 satellites), IRIDIUM 158 is designed to operate for up to 10 years, though the mission plans aim for a 15-year lifetime. The satellite uses two deployable solar arrays and batteries for power. It was manufactured by NGISGA and has a half hex prism shape with two panels.
der Satellit IRIDIUM 158 hinausgetragen 25.07.2018r. Durchschnittshöhe IRIDIUM 158 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 158 beträgt 26856.99 km/h. Neigung IRIDIUM 158 Satelliten 86.4°.