Iridium Next SV154 - Norad Identifikationsnummer: 43574
| Name im Katalog Spacetrack | IRIDIUM 154 |
| Alternative Bezeichnung | Iridium Next SV154 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 154 | IRIDIUM 154 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 154 | Flugzeiten IRIDIUM 154 |
| 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 154 | 789.86 km |
IRIDIUM 154, also known as Iridium Next SV154, is a communication and traffic monitoring satellite operated by IRIDS (Iridium LLC). Launched on July 25, 2018, from AFWTR SLC4E using a Falcon 9 launch vehicle, the satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans up to 9.4 meters when fully deployed. It is equipped with an L-band payload, Ka-band cross-links and downlinks, as well as ADS-B (Automatic Dependent Surveillance?Broadcast) and AIS (Automatic Identification System) receivers for traffic monitoring. 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, with an operational design lifetime of 10 years but planned to last up to 15 years. Manufactured by NGISGA (Northrop Grumman Innovation Systems), the satellite has a half hex prism shape with two panels and supports communication services as part of its mission objectives.
der Satellit IRIDIUM 154 hinausgetragen 25.07.2018r. Durchschnittshöhe IRIDIUM 154 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 154 beträgt 26856.98 km/h. Neigung IRIDIUM 154 Satelliten 86.4°.