IRIDIUM 165
Satellite information IRIDIUM 165 - Iridium Next SV165
| Spacetrack Directory Name | IRIDIUM 165 |
| Alternative name | Iridium Next SV165 |
| Group | IRIDIUM |
| Follow IRIDIUM 165 | IRIDIUM 165 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 165 | Pass predictions IRIDIUM 165 |
| Orbit launches |
2018-07-25 (8 years ago)
|
| Days in orbit | 2999 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| WWW | Here |
| Categories | |
| Perigee | 776 km |
| Apogee | 779 km |
| Orbit slope (inclination) | 86.4° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 165 | 789.86 km |
Additional information IRIDIUM 165
IRIDIUM 165, also known as Iridium Next SV165, is a communication and traffic monitoring satellite operated by IRIDS (Iridium LLC). It was launched on July 25, 2018, from Vandenberg Air Force Base using a Falcon 9 launch vehicle. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters when its components are fully deployed. Its dry mass is 700 kg, and it has a launch mass of 860 kg. Equipped with an L-band payload for communication, Ka-band cross-links, downlinks, ADS-B payload, and an AIS-receiver (on 58 satellites), IRIDIUM 165 relies on two deployable solar arrays and batteries for power. The satellites configuration is based on the ELiTeBus-1000 bus manufactured by NGISGA and designed to have a lifetime of up to 10 years with plans for extended operations up to 15 years.
satellite IRIDIUM 165 Date of exalting 25.07.2018y. Average height of ISS IRIDIUM 165 hundred 789.86 km. Average velocity IRIDIUM 165 is 26856.98 km/h. Inclination IRIDIUM 165 satellite 86.4°.TLE
Average velocity IRIDIUM 165
Average inclination IRIDIUM 165
Mean right ascension of the ascending node (RAAN) IRIDIUM 165
Mean argument of perigee IRIDIUM 165
Mean semi-major axis of the orbit IRIDIUM 165
Mean orbital eccentricity IRIDIUM 165
ISS
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