OCSE
Optical Calibration Sphere Experiment
General
| Designation | 26062 / 00004B |
| Launch date | 27 Jan 2000 |
| Country of origin | United States |
| Mission | Technology |
| Perigee/Apogee | 773 km |
| Inclination | 100° |
| Period | 100.4 min |
| Launch vehicle | Minotaur #1 |
Will be used to calibrer lasers at AFRL Starfire Optical Range
External resources
sat-index articles
Technical data
Specifications
| Prime contractor | L'Garde Inc |
| Platform | |
| Mass at launch | 22 kg |
| Mass in orbit | |
| Dimension | 3.5 m diameter (before inflation: 0.48 m long x 0.41 m diameter) |
| 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