Launch data:
| Designation | 17083 (see table) |
| Launch date | 23 Dec 2017 - 01:27 UT |
| Launch site | Va, SLC-4E |
| Launch vehicle | Falcon-9 v1.2 |
| Mission | Low orbit Communication, traffic monitoring |
Iridium-NEXT 116, 130-131, 134-135, 137-138, 141, 151, 153 |
USA |
Int. spacecraft nº: |
US spacecrafts nº: |
Launch data:
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| Prime manufacturer | Thales Alenia Space (prime), Orbital (integration) |
| Platform | ELiTeBus-1000 |
| Operator | Iridium Communications Inc. |
| Mass at launch | 860 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, AIS payload (on 58 satellites) |
| Solar array | 2 deployable solar arrays |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime | 15 years (planned) |
| SV 116 | SV 130 | SV 131 | SV 134 | SV 135 | SV 137 | SV 138 | SV 141 | SV 151 | SV 153 | ||
| Norad ID | 43072 | 43073 | 43079 | 43075 | 43070 | 43076 | 43071 | 43077 | 43074 | 43078 | |
| Int. code | 17083C | 17083D | 17083K | 17083F | 17083A | 17083G | 17083B | 17083H | 17083E | 17083J | |
| Earth orbit: | |||||||||||
| Perigee / Apogee | 609 X 626 km | ||||||||||
| Inclination | 86.7 deg | ||||||||||
| Period | min | ||||||||||
| Decay | 116 | 130 | 131 | 134 | 135 | 137 | 138 | 141 | 151 | 153 | |
| Ref.: #7(JR) - update: 23.01.18 | Home |