IRIDIUM 136
Satellite information IRIDIUM 136 - Iridium Next SV136
| Spacetrack Directory Name | IRIDIUM 136 |
| Alternative name | Iridium Next SV136 |
| Group | IRIDIUM |
| Follow IRIDIUM 136 | IRIDIUM 136 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 136 | Pass predictions IRIDIUM 136 |
| 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 136 | 789.86 km |
Additional information IRIDIUM 136
IRIDIUM 136, also known as Iridium Next SV136, is a communication and traffic monitoring satellite operated by IRIDS. It was launched on October 9, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. The spacecraft has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters with its deployable solar arrays. It weighs 860 kg at launch and 700 kg dry mass. Equipped with an L-band payload for communication, Ka-band cross-links, downlinks, ADS-B payload, and AIS-receiver, IRIDIUM 136 is part of a constellation designed to operate for up to 15 years. The satellite uses two deployable solar arrays and batteries for power.
satellite IRIDIUM 136 Date of exalting 09.10.2017y. Average height of ISS IRIDIUM 136 hundred 789.86 km. Average velocity IRIDIUM 136 is 26856.98 km/h. Inclination IRIDIUM 136 satellite 86.4°.TLE
Average velocity IRIDIUM 136
Average inclination IRIDIUM 136
Mean right ascension of the ascending node (RAAN) IRIDIUM 136
Mean argument of perigee IRIDIUM 136
Mean semi-major axis of the orbit IRIDIUM 136
Mean orbital eccentricity IRIDIUM 136
ISS
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