IGS 1A
Optical 1
General
| Designation | 27698 / 03009A |
| Launch date | 28 Mar 2003 |
| Country of origin | Japan |
| Mission | Military: reconnaissance |
| Perigee/Apogee | 500 km, sun-synchronous |
| Inclination | 97.3° |
| Period | (4-day revisit) |
| Launch vehicle | H2A #12 |
Optical satellite, 1-m resolution
Morning pass over North Korea
End of life
| Decay | 18 Jul 2014 |
External resources
sat-index articles
Technical data
Specifications
| Prime contractor | Mitsubishi Electric |
| Platform | |
| Mass at launch | 850 kg |
| Mass in orbit | |
| 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