Iridium Next SV133 - Norad Identifikationsnummer: 42955
| Name im Katalog Spacetrack | IRIDIUM 133 |
| Alternative Bezeichnung | Iridium Next SV133 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 133 | IRIDIUM 133 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 133 | Flugzeiten IRIDIUM 133 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3289 |
| 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 133 | 789.86 km |
IRIDIUM 133, also known as Iridium Next SV133, is a communication and traffic monitoring satellite owned by IRIDS and manufactured by OATKGA. Launched on October 9, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle, the satellite has a design life of 10 years with plans for an extended operation up to 15 years. It measures 3.1 meters in length and 1.5 meters in diameter, with a span of 9.4 meters. The dry mass is recorded at 700 kilograms, while the launch mass was 860 kilograms. Equipped with L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and an AIS-receiver, it utilizes two deployable solar arrays and batteries for power supply. Its shape is described as a half hex prism with two panels.
der Satellit IRIDIUM 133 hinausgetragen 09.10.2017r. Durchschnittshöhe IRIDIUM 133 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 133 beträgt 26856.99 km/h. Neigung IRIDIUM 133 Satelliten 86.4°.