IRIDIUM 134
Satellite information IRIDIUM 134 - Iridium Next SV134
| Spacetrack Directory Name | IRIDIUM 134 |
| Alternative name | Iridium Next SV134 |
| Group | IRIDIUM |
| Follow IRIDIUM 134 | IRIDIUM 134 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 134 | Pass predictions IRIDIUM 134 |
| 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 134 | 789.86 km |
Additional information IRIDIUM 134
IRIDIUM 134, also known as Iridium Next SV134, is a communication and traffic monitoring satellite manufactured by OATKGA for IRIDS (Iridium LLC). Launched on December 23, 2017, from the AFWTR SLC4E launch pad using a Falcon 9 rocket, this satellite has a BUS of EliteBus with the configuration ELiTeBus-1000. It measures 3.1 meters in length and 1.5 meters in diameter with a span of 9.4 meters. The dry mass is recorded at 700 kg while its launch mass was 860 kg. Equipped with deployable solar arrays and batteries for power, the satellite carries an L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, and AIS-receiver (part of a group of 58 satellites). The satellites design lifetime is ten years, with plans extending its operational life to fifteen years. Its shape is described as Half Hex Prism+2 pan.
satellite IRIDIUM 134 Date of exalting 23.12.2017y. Average height of ISS IRIDIUM 134 hundred 789.86 km. Average velocity IRIDIUM 134 is 26856.99 km/h. Inclination IRIDIUM 134 satellite 86.4°.TLE
Average velocity IRIDIUM 134
Average inclination IRIDIUM 134
Mean right ascension of the ascending node (RAAN) IRIDIUM 134
Mean argument of perigee IRIDIUM 134
Mean semi-major axis of the orbit IRIDIUM 134
Mean orbital eccentricity IRIDIUM 134
ISS
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