Iridium-NEXT 140, 142-146, 148-150, 157 |
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 140 | SV 142 | SV 143 | SV 144 | SV 145 | SV 146 | SV 148 | SV 149 | SV 150 | SV 157 | ||
| Norad ID | 43252 | 43257 | 43258 | 43255 | 43253 | 43254 | 43249 | 43250 | 43256 | 43251 | |
| Int. code | 18030D | 18030J | 18030K | 18030G | 18030E | 18030F | 18030A | 18030B | 18030H | 18030C | |
| Earth orbit: | |||||||||||
| Perigee / Apogee | 608 X 626 km | ||||||||||
| Inclination | 86.7 deg | ||||||||||
| Period | 100.4 min | ||||||||||
| Decay | 140 | 142 | 143 | 144 | 145 | 146 | 148 | 149 | 150 | 157 | |
| Ref.: #7(JR747), #228 - update: 01.07.18 | Home |