Iridium Next SV136 - Norad Identifikationsnummer: 42962
| Name im Katalog Spacetrack | IRIDIUM 136 |
| Alternative Bezeichnung | Iridium Next SV136 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 136 | IRIDIUM 136 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 136 | Flugzeiten IRIDIUM 136 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3288 |
| 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 136 | 789.86 km |
IRIDIUM 136, also known as Iridium Next SV136, is a communication and traffic monitoring satellite operated by IRIDS. It was launched on October 9, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. The spacecraft has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters with its deployable solar arrays. It weighs 860 kg at launch and 700 kg dry mass. Equipped with an L-band payload for communication, Ka-band cross-links, downlinks, ADS-B payload, and AIS-receiver, IRIDIUM 136 is part of a constellation designed to operate for up to 15 years. The satellite uses two deployable solar arrays and batteries for power.
der Satellit IRIDIUM 136 hinausgetragen 09.10.2017r. Durchschnittshöhe IRIDIUM 136 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 136 beträgt 26856.98 km/h. Neigung IRIDIUM 136 Satelliten 86.4°.