IRIDIUM 146
Satellite information IRIDIUM 146 - Iridium Next SV146
| Spacetrack Directory Name | IRIDIUM 146 |
| Alternative name | Iridium Next SV146 |
| Group | IRIDIUM |
| Follow IRIDIUM 146 | IRIDIUM 146 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 146 | Pass predictions IRIDIUM 146 |
| Orbit launches |
2018-03-30 (8 years ago)
|
| Days in orbit | 3116 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| Categories | |
| Perigee | 776 km |
| Apogee | 779 km |
| Orbit slope (inclination) | 86.39° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 146 | 789.86 km |
Additional information IRIDIUM 146
IRIDIUM 146, also known as Iridium Next SV146, is a communication and traffic monitoring satellite owned by IRIDS and launched on March 30, 2018, from AFWTR SLC4E using the Falcon 9 launch vehicle. It has a configuration of ELiTeBus-1000 with dimensions including a length of 3.1 meters, diameter of 1.5 meters, and span of 9.4 meters. The satellites dry mass is 700 kilograms and its launch mass was 860 kilograms. It carries L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and an AIS-receiver (part of a set on 58 satellites). Power is provided by two deployable solar arrays and batteries. Its shape is described as Half Hex Prism+2 pan, with a planned operational lifetime of up to 15 years beyond its designed lifespan of 10 years. The satellite was manufactured by OATKGA for communication purposes and traffic monitoring.
satellite IRIDIUM 146 Date of exalting 30.03.2018y. Average height of ISS IRIDIUM 146 hundred 789.86 km. Average velocity IRIDIUM 146 is 26856.99 km/h. Inclination IRIDIUM 146 satellite 86.4°.TLE
Average velocity IRIDIUM 146
Average inclination IRIDIUM 146
Mean right ascension of the ascending node (RAAN) IRIDIUM 146
Mean argument of perigee IRIDIUM 146
Mean semi-major axis of the orbit IRIDIUM 146
Mean orbital eccentricity IRIDIUM 146
ISS
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