Nexsat 1
General
| Designation | / 24024 |
| Launch date | 3 Feb 2024 |
| Country of origin | Egypt |
| Mission | Remote sensing |
| Perigee/Apogee | 511/524 km |
| Inclination | 97.4° |
| Period | 94.8 min |
| Launch vehicle | Smart Dragon 3 #4 |
Two cameras with best resolution of 7.5 m with a 30 km swath width.
Technical data
Specifications
| Prime contractor | NARSS (Egypt) |
| Platform | |
| Mass at launch | 65 kg |
| Dry mass | |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime | 5 years |
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V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly
V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly