IRIDIUM 167
Satellite information IRIDIUM 167 - Iridium Next SV167
| Spacetrack Directory Name | IRIDIUM 167 |
| Alternative name | Iridium Next SV167 |
| Group | IRIDIUM |
| Follow IRIDIUM 167 | IRIDIUM 167 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 167 | Pass predictions IRIDIUM 167 |
| Orbit launches |
2019-01-11 (7 years ago)
|
| Days in orbit | 2829 |
| 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) | 86.39° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 167 | 789.86 km |
Additional information IRIDIUM 167
IRIDIUM 167, also known as Iridium Next SV167, is a communication and traffic monitoring satellite owned by IRIDS and manufactured by NGISGA. Launched on January 11, 2019, from AFWTR using the Falcon 9 launch vehicle, it has a configuration of ELiTeBus-1000 with dimensions: length 3.1 meters, diameter 1.5 meters, and span 9.4 meters. The satellites dry mass is 700 kg, while its launch mass was 860 kg. It is equipped with an L-band payload, Ka-band cross-links and downlinks, as well as ADS-B payload and AIS-receiver. Its power system includes two deployable solar arrays and batteries. Designed for a ten-year lifespan but planned for fifteen years of operation, the satellites shape is described as a half hex prism with two panels.
satellite IRIDIUM 167 Date of exalting 11.01.2019y. Average height of ISS IRIDIUM 167 hundred 789.86 km. Average velocity IRIDIUM 167 is 26856.98 km/h. Inclination IRIDIUM 167 satellite 86.4°.TLE
Average velocity IRIDIUM 167
Average inclination IRIDIUM 167
Mean right ascension of the ascending node (RAAN) IRIDIUM 167
Mean argument of perigee IRIDIUM 167
Mean semi-major axis of the orbit IRIDIUM 167
Mean orbital eccentricity IRIDIUM 167
ISS
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