Iridium-NEXT 110, 147, 152, 161-162 |
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 | |
| 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 110 | SV 147 | SV 152 | SV 161 | SV 162 | ||
| Norad ID | 43481 | 43480 | 43479 | 43478 | 43482 | |
| Int. code | 18047F | 18047E | 18047D | 18047C | 18047G | |
| Earth orbit: | ||||||
| Perigee / Apogee | 488x718 km | 489x714 km | 493x710 km | 489x714 km | 491x715 km | |
| Inclination | 86.7 deg | |||||
| Period | min | |||||
| Decay | 110 | 147 | 152 | 161 | 162 | |
| Ref.: #7(JR749), #228 - update: 20.11.18 | Home |