Orbital Express NextSat
General
| Designation | 30774 / 07006C |
| Launch date | 9 Mar 2007 |
| Country of origin | United States |
| Mission | Experimental |
| Perigee/Apogee | 491/499 km |
| Inclination | 46° |
| Period | 94.5 min |
| Launch vehicle | Atlas 5 #9 |
See details in Orbital Express Astro
The satellite operated very well in the first month.
End of life
| Decay | 21 Apr 2023 |
sat-index articles
Technical data
Specifications
| Prime contractor | Ball Aerospace |
| Platform | |
| Mass at launch | 226 kg |
| Dry mass | |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |
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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