Iridium Next SV104 - Norad Identifikationsnummer: 41922
| Name im Katalog Spacetrack | IRIDIUM 104 |
| Alternative Bezeichnung | Iridium Next SV104 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 104 | IRIDIUM 104 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 104 | Flugzeiten IRIDIUM 104 |
| 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 104 | 789.86 km |
The satellite IRIDIUM 104 (also known as Iridium Next SV104) has a NORAD catalog ID of 41922 and an OBJECT_ID of 2017-003F. Launched on January 14, 2017, from AFWTR using SLC4E with the launch vehicle Falcon 9, this satellite is part of a US project for communication and traffic monitoring purposes. It measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters. The dry mass of IRIDIUM 104 is 700 kg, while the launch mass was 860 kg. It is equipped with L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver technology (part of a constellation featuring this equipment on 58 satellites). Power comes from two deployable solar arrays and batteries, and its shape is described as Half Hex Prism+2 pan. The satellites configuration is ELiTeBus-1000, manufactured by OATKGA with a designed lifetime of 10 years but planned for up to 15 years.
der Satellit IRIDIUM 104 hinausgetragen 14.01.2017r. Durchschnittshöhe IRIDIUM 104 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 104 beträgt 26856.99 km/h. Neigung IRIDIUM 104 Satelliten 86.4°.