BY70-1 |
China |
Int. spacecraft nº: |
Chinese spacecraft nº: 323 |
| Designation | 41909 / 16083C |
| Launch date | 28 Dec 2016 - 03:23 UT |
| Launch site | Taiyuan, LC9 |
| Launch vehicle | CZ-2D |
| Mission | Communication |
| Earth orbit: | |
| Perigee / Apogee | 212 x 523 km |
| Eccentricity | |
| Inclination | 97.6° |
| Period | min |
| Prime manufacturer | |
| Platform | 2U CubeSat |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Uplink (MHz) | 145.920 |
| Downlink (MHz) | 436.200 |
| Beacon (MHz) | 436.200 |
| Mode | 9600bps BPSK FM_tone 67.0Hz |
| Re-entered date: | 18 Feb 2017 - .01 |
| Lifetime: |
| Ref.: #3(SD532), #7(JR733), #228 - update: 30.06.17 | Home |