IRIDIUM 124
Satellite information IRIDIUM 124 - Iridium Next SV124
| Spacetrack Directory Name | IRIDIUM 124 |
| Alternative name | Iridium Next SV124 |
| Group | IRIDIUM |
| Follow IRIDIUM 124 | IRIDIUM 124 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 124 | Pass predictions IRIDIUM 124 |
| Orbit launches |
2017-06-25 (9 years ago)
|
| Days in orbit | 3394 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| Categories | |
| Perigee | 746 km |
| Apogee | 749 km |
| Orbit slope (inclination) | 86.45° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 124 | 759.88 km |
Additional information IRIDIUM 124
IRIDIUM 124, also known as Iridium Next SV124, is a communication and traffic monitoring satellite operated by IRIDS (Iridium LLC). Launched on June 25, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle, the satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. It is equipped with an L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and AIS-receiver (on 58 satellites), and its configuration is based on the ELiTeBus-1000 bus manufactured by OATKGA. The satellite has a launch mass of 860 kg and a dry mass of 700 kg, powered by two deployable solar arrays and batteries. Its designed lifetime is 10 years with a planned extension to 15 years.
satellite IRIDIUM 124 Date of exalting 25.06.2017y. Average height of ISS IRIDIUM 124 hundred 759.88 km. Average velocity IRIDIUM 124 is 26913.34 km/h. Inclination IRIDIUM 124 satellite 86.45°.TLE
Average velocity IRIDIUM 124
Average inclination IRIDIUM 124
Mean right ascension of the ascending node (RAAN) IRIDIUM 124
Mean argument of perigee IRIDIUM 124
Mean semi-major axis of the orbit IRIDIUM 124
Mean orbital eccentricity IRIDIUM 124
ISS
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