Iridium Next SV170 - Norad Identifikationsnummer: 43930
| Name im Katalog Spacetrack | IRIDIUM 170 |
| Alternative Bezeichnung | Iridium Next SV170 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 170 | IRIDIUM 170 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 170 | Flugzeiten IRIDIUM 170 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 2829 |
| 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 | 652 km |
| Apogäum | 655 km |
| Neigung der Umlaufbahn (Inklination) | 86.61° |
| Runden pro Tag | 15 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 170 | 666.11 km |
IRIDIUM 170, also known as Iridium Next SV170, is a communication and traffic monitoring satellite designed by NGISGA for IRIDS (Iridium). It was launched on January 11, 2019, from AFWTRs SLC4E pad using a Falcon 9 launch vehicle. The satellite features a configuration known as ELiTeBus-1000 with dimensions of 3.1 meters in length and 1.5 meters in diameter, spanning 9.4 meters. It has a dry mass of 700 kilograms and was launched with an overall mass of 860 kilograms. Equipped with L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receivers (present on 58 satellites), IRIDIUM 170 utilizes two deployable solar arrays and batteries for power supply. The satellite is expected to have a design lifetime of 10 years, with plans for an extended operational life of up to 15 years.
der Satellit IRIDIUM 170 hinausgetragen 11.01.2019r. Durchschnittshöhe IRIDIUM 170 Text Nummer 1: das. 666.11 km. Durchschnittsgeschwindigkeit IRIDIUM 170 beträgt 27091.91 km/h. Neigung IRIDIUM 170 Satelliten 86.61°.