Iridium Next SV152 - Norad Identifikationsnummer: 43479
| Name im Katalog Spacetrack | IRIDIUM 152 |
| Alternative Bezeichnung | Iridium Next SV152 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 152 | IRIDIUM 152 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 152 | Flugzeiten IRIDIUM 152 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3063 |
| 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 152 | 789.86 km |
IRIDIUM 152, also known as Iridium Next SV152, is a communication and traffic monitoring satellite operated by IRIDS (Iridium LLC). Launched on May 22, 2018, from AFWTR SLC4E using a Falcon 9 launch vehicle, it has dimensions of 3.1 meters in length, 1.5 meters in diameter, and a span of 9.4 meters. The satellite is equipped with a deployable solar array system and batteries for power supply. It features an L-band payload, Ka-band cross-links and downlinks, as well as ADS-B and AIS-receiver payloads (on 58 satellites). With a dry mass of 700 kg and a launch mass of 860 kg, it was manufactured by OATKGA (Orbital ATK) and is designed to operate for up to 15 years. The satellite has a half hex prism shape with two panels and its configuration is based on the ELiTeBus-1000 bus system.
der Satellit IRIDIUM 152 hinausgetragen 22.05.2018r. Durchschnittshöhe IRIDIUM 152 Text Nummer 1: das. 789.86 km. Durchschnittsgeschwindigkeit IRIDIUM 152 beträgt 26856.99 km/h. Neigung IRIDIUM 152 Satelliten 86.4°.