Iridium Next SV130 - Norad Identifikationsnummer: 43073
| Name im Katalog Spacetrack | IRIDIUM 130 |
| Alternative Bezeichnung | Iridium Next SV130 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 130 | IRIDIUM 130 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 130 | Flugzeiten IRIDIUM 130 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3213 |
| 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 130 | 789.86 km |
IRIDIUM 130, also known as Iridium Next SV130, is a communication and traffic monitoring satellite owned by IRIDS and manufactured by OATKGA. Launched on December 23, 2017, from AFWTR using a Falcon 9 launch vehicle from SLC4E, it has dimensions of 3.1 meters in length and 1.5 meters in diameter with a span of 9.4 meters. The satellite has a dry mass of 700 kg and a launch mass of 860 kg. Equipped with L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and an AIS-receiver (on 58 satellites), it relies on two deployable solar arrays and batteries for power. Designed to operate for 10 years but planned for a 15-year lifespan, the satellite has a half hex prism shape with two panels and operates in a constellation setup without specific mention of its constellation name or related satellites.
der Satellit IRIDIUM 130 hinausgetragen 23.12.2017r. Durchschnittshöhe IRIDIUM 130 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 130 beträgt 26856.99 km/h. Neigung IRIDIUM 130 Satelliten 86.4°.
W tabelce, częstotliwości. IRIDIUM 130.
| Downlink | Modus |
|---|---|
| 1623.192 MHz | FM |