IRIDIUM 109
Satellite information IRIDIUM 109 - Iridium Next SV109
| Spacetrack Directory Name | IRIDIUM 109 |
| Alternative name | Iridium Next SV109 |
| Group | IRIDIUM |
| Follow IRIDIUM 109 | IRIDIUM 109 Tracker |
| Group follow IRIDIUM | Tracker IRIDIUM |
| Pass predictions IRIDIUM 109 | Pass predictions IRIDIUM 109 |
| Orbit launches |
2017-01-14 (9 years ago)
|
| Days in orbit | 3556 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| Categories | |
| Perigee | 776 km |
| Apogee | 779 km |
| Orbit slope (inclination) | 86.4° |
| Laps per day | 14 |
| Orbit | LEO (Polar) |
| Height IRIDIUM 109 | 789.86 km |
Additional information IRIDIUM 109
The satellite IRIDIUM 109 (also known as Iridium Next SV109) was launched on January 14, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. It is owned by IRIDS and manufactured by OATKGA for communication and traffic monitoring purposes. The satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. Its dry mass is 700 kg with a launch mass of 860 kg. It features an L-band payload, Ka-band cross-links and downlinks, and ADS-B and AIS-receiver payloads (on 58 satellites). The satellites power source consists of two deployable solar arrays and batteries. Its design life is projected to be up to 15 years with a configuration known as ELiTeBus-1000.
satellite IRIDIUM 109 Date of exalting 14.01.2017y. Average height of ISS IRIDIUM 109 hundred 789.86 km. Average velocity IRIDIUM 109 is 26856.98 km/h. Inclination IRIDIUM 109 satellite 86.4°.TLE
Average velocity IRIDIUM 109
Average inclination IRIDIUM 109
Mean right ascension of the ascending node (RAAN) IRIDIUM 109
Mean argument of perigee IRIDIUM 109
Mean semi-major axis of the orbit IRIDIUM 109
Mean orbital eccentricity IRIDIUM 109
ISS
Buy us a coffee!
