Iridium-NEXT 107, 119, 122, 125, 127, 129, 132-133, 136, 139 |
USA |
Int. spacecraft nº: |
US spacecrafts nº: |
| Designation | 17061 (see table) |
| Launch date | 09 Oct 2017 - 12:37 UT |
| Launch site | Va, SLC-4E |
| Launch vehicle | Falcon-9 v1.2 |
| Mission | Low orbit Communication |
| Prime manufacturer | |
| Platform | |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| SV 107 | SV 119 | SV 122 | SV 125 | SV 127 | SV 129 | SV 132 | SV 133 | SV 136 | SV 139 | ||
| Norad ID | 42960 | 42959 | 42957 | 42964 | 42956 | 42958 | 42961 | 42955 | 42962 | 42963 | |
| Int. code | 17061F | 17061E | 17061C | 1706K | 17061B | 17061D | 17061G | 17061A | 17061H | 17061J | |
| Earth orbit: | |||||||||||
| Perigee / Apogee | 612 x 626 km | 612 x 626 km | 612 x 626 km | 612 x 626 km | 612 x 626 km | 612 x 626 km | 612 x 626 km | 612 x 626 km | 612 x 626 km | 612 x 626 km | |
| Inclination | deg | deg | deg | deg | deg | deg | deg | deg | deg | deg | |
| Period | 86.6 min | 86.6 min | 86.6 min | 86.6 min | 86.6 min | 86.6 min | 86.6 min | 86.6 min | 86.6 min | 86.6 min | |
| Decay | 107 | 119 | 122 | 125 | 127 | 129 | 132 | 133 | 136 | 139 | |
| Ref.: #7(JR742) - update: 30.11.17 | Home |