IRIDIUM 135
Satellite information IRIDIUM 135 - Iridium Next SV135
| Spacetrack Directory Name | IRIDIUM 135 |
| Alternative name | Iridium Next SV135 |
| Group | IRIDIUM |
| Follow IRIDIUM 135 | IRIDIUM 135 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 135 | Pass predictions IRIDIUM 135 |
| 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 135 | 789.86 km |
Additional information IRIDIUM 135
The satellite IRIDIUM 135 (also known as Iridium Next SV135) was launched on December 23, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. It is owned by IRIDS and manufactured by OATKGA. The satellites configuration is ELiTeBus-1000 with dimensions of 3.1 meters in length, 1.5 meters in diameter, and a span of 9.4 meters. Its dry mass is 700 kg, while the launch mass was 860 kg. Equipped with an L-band payload, Ka-band cross-links and downlinks, and ADS-B payload (along with AIS-receiver on some satellites), it serves communication and traffic monitoring purposes. The satellites power source includes two deployable solar arrays and batteries. Its design lifetime is planned for up to 15 years, though the designed lifespan is 10 years.
satellite IRIDIUM 135 Date of exalting 23.12.2017y. Average height of ISS IRIDIUM 135 hundred 789.86 km. Average velocity IRIDIUM 135 is 26856.98 km/h. Inclination IRIDIUM 135 satellite 86.4°.TLE
Average velocity IRIDIUM 135
Average inclination IRIDIUM 135
Mean right ascension of the ascending node (RAAN) IRIDIUM 135
Mean argument of perigee IRIDIUM 135
Mean semi-major axis of the orbit IRIDIUM 135
Mean orbital eccentricity IRIDIUM 135
ISS
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