Iridium Next SV102 - Norad Identifikationsnummer: 41920
| Name im Katalog Spacetrack | IRIDIUM 102 |
| Alternative Bezeichnung | Iridium Next SV102 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 102 | IRIDIUM 102 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 102 | Flugzeiten IRIDIUM 102 |
| 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 102 | 789.86 km |
IRIDIUM 102 (also known as Iridium Next SV102) is a communication and traffic monitoring satellite launched on January 14, 2017, from AFWTR 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 when its solar arrays are deployed. It weighs 860 kilograms at launch and 700 kilograms dry mass. Equipped with an L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver, IRIDIUM 102 is part of a constellation designed for communication and traffic monitoring purposes. It has a planned operational lifetime of up to 15 years and uses two deployable solar arrays and batteries for power. The satellites shape is described as half hexagonal prism with two pans, and it was manufactured by OATKGA on behalf of IRIDS (Iridium).
der Satellit IRIDIUM 102 hinausgetragen 14.01.2017r. Durchschnittshöhe IRIDIUM 102 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 102 beträgt 26856.99 km/h. Neigung IRIDIUM 102 Satelliten 86.4°.