Iridium Next SV135 - Norad Identifikationsnummer: 43070
| Name im Katalog Spacetrack | IRIDIUM 135 |
| Alternative Bezeichnung | Iridium Next SV135 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 135 | IRIDIUM 135 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 135 | Flugzeiten IRIDIUM 135 |
| In die Umlaufbahn bringen |
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| 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 135 | 789.86 km |
The satellite IRIDIUM 135 (also known as Iridium Next SV135) was launched on December 23, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. It is owned by IRIDS and manufactured by OATKGA. The satellites configuration is ELiTeBus-1000 with dimensions of 3.1 meters in length, 1.5 meters in diameter, and a span of 9.4 meters. Its dry mass is 700 kg, while the launch mass was 860 kg. Equipped with an L-band payload, Ka-band cross-links and downlinks, and ADS-B payload (along with AIS-receiver on some satellites), it serves communication and traffic monitoring purposes. The satellites power source includes two deployable solar arrays and batteries. Its design lifetime is planned for up to 15 years, though the designed lifespan is 10 years.
der Satellit IRIDIUM 135 hinausgetragen 23.12.2017r. Durchschnittshöhe IRIDIUM 135 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 135 beträgt 26856.98 km/h. Neigung IRIDIUM 135 Satelliten 86.4°.