Iridium Next SV115 - Norad Identifikationsnummer: 42806
| Name im Katalog Spacetrack | IRIDIUM 115 |
| Alternative Bezeichnung | Iridium Next SV115 |
| Gruppe | IRIDIUM |
| Folge IRIDIUM 115 | IRIDIUM 115 Tracker |
| Folge der Gruppe. IRIDIUM | Tracker IRIDIUM |
| Flugzeiten IRIDIUM 115 | Flugzeiten IRIDIUM 115 |
| In die Umlaufbahn bringen |
|
| Tage im Orbit | 3394 |
| Herkunftsland/-organisation | USA (US) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | AFWTR (Vandenberg Air Force Base, USA) |
| Typ | Satellit |
| Kategorie | |
| Perygeum | 745 km |
| Apogäum | 750 km |
| Neigung der Umlaufbahn (Inklination) | 86.44° |
| Runden pro Tag | 14 |
| Orbit | LEO (Polar) |
| Höhe IRIDIUM 115 | 759.88 km |
IRIDIUM 115, also known as Iridium Next SV115, is a communication and traffic monitoring satellite launched on June 25, 2017, from Vandenberg Air Force Base (AFWTR) using Falcon 9 as the launch vehicle. It was manufactured by OATKGA and has a design lifetime of 10 years with plans for an extended operation up to 15 years. The satellite measures 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters when its solar arrays are deployed. Its dry mass is 700 kilograms while the launch mass was 860 kilograms. Equipped with an L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and AIS-receiver, IRIDIUM 115 operates within a configuration known as ELiTeBus-1000. The satellites power is provided by two deployable solar arrays along with batteries. It is owned by IRIDS and falls under the BUS category of EliteBus.
der Satellit IRIDIUM 115 hinausgetragen 25.06.2017r. Durchschnittshöhe IRIDIUM 115 Text Nummer 1: das. 759.88 km. Durchschnittsgeschwindigkeit IRIDIUM 115 beträgt 26913.35 km/h. Neigung IRIDIUM 115 Satelliten 86.45°.