Iridium-NEXT 154-156, 158-160, 163-166 |
USA |
Int. spacecraft nº: |
US spacecrafts nº: |
Launch data:
|
|
| 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 154 | SV 155 | SV 156 | SV 158 | SV 159 | SV 160 | SV 163 | SV 164 | SV 165 | SV 166 | ||
| Norad ID | 43574 | 43573 | 43576 | 43571 | 43578 | 43569 | 43575 | 43577 | 43572 | 43570 | |
| Int. code | 18061F | 18061E | 18061H | 18061C | 18061K | 18061A | 18061G | 18061J | 18061D | 18061B | |
| Earth orbit: | |||||||||||
| Perigee / Apogee | 608 x 623 km | 608 x 623 km | 608 x 623 km | 607 x 623 km | 608 x 623 km | 607 x 623 km | 607 x 623 km | 607 x 623 km | 607 x 623 km | 608 x 623 km | |
| Inclination | 86.7 deg | ||||||||||
| Period | min | ||||||||||
| Decay | 154 | 155 | 156 | 158 | 159 | 160 | 163 | 164 | 165 | 166 | |
| Ref.: #7(JR751) - update: 20.11.18 | Home |