IRIDIUM 137
Satellite information IRIDIUM 137 - Iridium Next SV137
| Spacetrack Directory Name | IRIDIUM 137 |
| Alternative name | Iridium Next SV137 |
| Group | IRIDIUM |
| Follow IRIDIUM 137 | IRIDIUM 137 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 137 | Pass predictions IRIDIUM 137 |
| Orbit launches |
2017-12-23 (8 years ago)
|
| Days in orbit | 3213 |
| 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 137 | 789.86 km |
Additional information IRIDIUM 137
IRIDIUM 137, also known as Iridium Next SV137, is a communication and traffic monitoring satellite operated by IRIDS. It was launched on December 23, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. The spacecraft measures 3.1 meters in length with a diameter of 1.5 meters and spans 9.4 meters when fully deployed. Weighing 860 kg at launch, its dry mass is 700 kg. It is equipped with L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and an AIS-receiver for traffic monitoring purposes. The satellites power source includes two deployable solar arrays and batteries. Its design aims for a 10-year operational lifetime with plans to extend up to 15 years. Manufactured by OATKGA, the satellite is part of the EliteBus configuration series.
satellite IRIDIUM 137 Date of exalting 23.12.2017y. Average height of ISS IRIDIUM 137 hundred 789.86 km. Average velocity IRIDIUM 137 is 26856.99 km/h. Inclination IRIDIUM 137 satellite 86.4°.TLE
Average velocity IRIDIUM 137
Average inclination IRIDIUM 137
Mean right ascension of the ascending node (RAAN) IRIDIUM 137
Mean argument of perigee IRIDIUM 137
Mean semi-major axis of the orbit IRIDIUM 137
Mean orbital eccentricity IRIDIUM 137
ISS
Buy us a coffee!
