OPS-SAT |
ESA |
Int. spacecraft nº: |
ESA spacecraft nº: 128 |
| Designation | 44878 / 19092F |
| Launch date | 18 Dec 2019 - 08:54 UTC |
| Launch site | Ko, ELS |
| Launch vehicle | Soyuz-ST-A Fregat-M |
| Mission | |
| Earth orbit: | |
| Perigee / Apogee | 508 x 527 km |
| Eccentricity | |
| Inclination | 97.4° |
| Period | 95.0 min |
| Prime manufacturer | TU Graz |
| Platform | 3U CubeSat |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | advanced flight computer |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR773), #228 - update: 20.01.20 | Home |