Iridium-NEXT 113, 115, 117, 118, 120, 121, 123, 124, 126, 128 |
USA |
Int. spacecraft nº: |
US spacecrafts nº: |
Launch data:
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| 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 |
| Solar array | 2 deployable solar arrays |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime | 10 years (design) |
| SV 113 | SV 115 | SV 117 | SV 118 | SV 120 | SV 121 | SV 123 | SV 124 | SV 126 | SV 128 | ||
| Norad ID | 42803 | 42806 | 42808 | 42807 | 42805 | 42812 | 42804 | 42810 | 42809 | 42811 | |
| Int. code | 17039A | 17039D | 17039F | 17039E | 17039C | 17039K | 17039B | 17039H | 17039G | 17039J | |
| Earth orbit: | |||||||||||
| Perigee / Apogee | 607 x 625 km | 607 x 625 km | 607 x 625 km | 607 x 625 km | 607 x 625 km | 609 x 625 km | 607 x 625 km | 608 x 625 km | 608 x 625 km | 608 x 625 km | |
| Inclination | 86.7 deg | 86.7 deg | 86.7 deg | 86.7 deg | 86.7 deg | 86.7 deg | 86.7 deg | 86.7 deg | 86.7 deg | 86.7 deg | |
| Period | min | min | min | min | min | min | min | min | min | min | |
| Decay | 34 | 35 | 36 | 37 | 38 | 39 | 40 | ||||
| Ref.: #7(JR739,740), #14 - update: 14.01.18 | Home |