IRIDIUM 139
Satellite information IRIDIUM 139 - Iridium Next SV139
| Spacetrack Directory Name | IRIDIUM 139 |
| Alternative name | Iridium Next SV139 |
| Group | IRIDIUM |
| Follow IRIDIUM 139 | IRIDIUM 139 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 139 | Pass predictions IRIDIUM 139 |
| 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 139 | 789.86 km |
Additional information IRIDIUM 139
IRIDIUM 139, also known as Iridium Next SV139, is a communication and traffic monitoring satellite built by OATKGA for IRIDS (Iridium LLC). Launched on October 9, 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 a span of 9.4 meters. It features an EliteBus configuration with a dry mass of 700 kg and was designed for a 10-year lifetime but planned for up to 15 years. Equipped with L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver, the satellite is powered by two deployable solar arrays and batteries. Its shape is described as Half Hex Prism+2 pan.
satellite IRIDIUM 139 Date of exalting 09.10.2017y. Average height of ISS IRIDIUM 139 hundred 789.86 km. Average velocity IRIDIUM 139 is 26856.99 km/h. Inclination IRIDIUM 139 satellite 86.4°.TLE
Average velocity IRIDIUM 139
Average inclination IRIDIUM 139
Mean right ascension of the ascending node (RAAN) IRIDIUM 139
Mean argument of perigee IRIDIUM 139
Mean semi-major axis of the orbit IRIDIUM 139
Mean orbital eccentricity IRIDIUM 139
ISS
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