IRIDIUM 125
Satellite information IRIDIUM 125 - Iridium Next SV125
| Spacetrack Directory Name | IRIDIUM 125 |
| Alternative name | Iridium Next SV125 |
| Group | IRIDIUM |
| Follow IRIDIUM 125 | IRIDIUM 125 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 125 | Pass predictions IRIDIUM 125 |
| Orbit launches |
2017-10-09 (9 years ago)
|
| Days in orbit | 3288 |
| 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 125 | 789.86 km |
Additional information IRIDIUM 125
The IRIDIUM 125 satellite, also known as Iridium Next SV125, was launched on October 9, 2017, from the AFWTR launch site using a Falcon 9 vehicle. It is owned by IRIDS and manufactured by OATKGA with a design lifetime of 10 years but planned for up to 15 years. The satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters, featuring the EliteBus configuration. It weighs 860 kg at launch and carries equipment including an L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver technology. Its purpose is communication and traffic monitoring, powered by two deployable solar arrays and batteries. The satellites shape is described as a half hex prism with two panels.
satellite IRIDIUM 125 Date of exalting 09.10.2017y. Average height of ISS IRIDIUM 125 hundred 789.86 km. Average velocity IRIDIUM 125 is 26856.99 km/h. Inclination IRIDIUM 125 satellite 86.4°.TLE
Average velocity IRIDIUM 125
Average inclination IRIDIUM 125
Mean right ascension of the ascending node (RAAN) IRIDIUM 125
Mean argument of perigee IRIDIUM 125
Mean semi-major axis of the orbit IRIDIUM 125
Mean orbital eccentricity IRIDIUM 125
ISS
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