Asnaro 2
Advanced Satellite with New system ARchitecture for Observation
General
| Designation | 43152 / 18007A |
| Launch date | 17 Jan 2018 |
| Country of origin | Japan |
| Mission | Remote sensing |
| Perigee/Apogee | 500 km |
| Inclination | 97.5° |
| Period | 94.8 min |
| Launch vehicle | Epsilon #3 |
sat-index articles
Technical data
Specifications
| Prime contractor | |
| Platform | Nextar NX-300L |
| Mass at launch | 570 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