Iridium Next SV114 - Norad Identifikationsnummer: 41923
| Name im Katalog Spacetrack | IRIDIUM 114 |
| Alternative Bezeichnung | Iridium Next SV114 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 114 | IRIDIUM 114 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 114 | Flugzeiten IRIDIUM 114 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3556 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Typ | Satellit |
| Kategorie | |
| Perygeum | 776 km |
| Apogäum | 779 km |
| Neigung der Umlaufbahn (Inklination) | 86.4° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 114 | 789.86 km |
IRIDIUM 114, also known as Iridium Next SV114, is a communication and traffic monitoring satellite owned by IRIDS (Iridium LLC) and manufactured by OATKGA. It was launched on January 14, 2017, from the AFWTR at SLC4E using a Falcon 9 launch vehicle. The satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. Its dry mass is 700 kg, and it weighs 860 kg at launch. It is equipped with L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver technology for communication and traffic monitoring purposes. IRIDIUM 114 has a design lifetime of 10 years but aims to operate up to 15 years. Its power source includes two deployable solar arrays and batteries. The satellites shape is described as a Half Hex Prism with 2 pans, and its radar cross-section (RCS) is measured at 2.4372 m?.
der Satellit IRIDIUM 114 hinausgetragen 14.01.2017r. Durchschnittshöhe IRIDIUM 114 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 114 beträgt 26856.99 km/h. Neigung IRIDIUM 114 Satelliten 86.4°.