Iridium-NEXT 167-173, 175-176, 180 |
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) |
| SV167 | SV168 | SV169 | SV170 | SV171 | SV172 | SV173 | SV175 | SV176 | SV180 | ||
| Norad ID | 43931 | 43924 | 43926 | 43930 | 43929 | 43927 | 43925 | 43928 | 43923 | 43922 | |
| Int. code | 19002K | 19002C | 19002E | 19002J | 19002H | 19002F | 19002D | 19002G | 19002B | 19002A | |
| Earth orbit: | |||||||||||
| Perigee / Apogee | 611 x 623 km | ||||||||||
| Inclination | 86.7 deg | ||||||||||
| Period | min | ||||||||||
| Decay | 167 | 168 | 169 | 170 | 171 | 172 | 173 | 175 | 176 | 180 | |
| Ref.: #7(JR760,761) - update: 15.03.19 | Home |