View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 40043U 26134.69647705 +.00000000 +00000-0 +16208-3 0 00004
2 40043 97.7792 285.4873 0049422 182.8795 177.2143 14.85012026 06
| Epoch (UTC): | 14 May 2026 16:42:55 |
| Eccentricity: | 0.0049422 |
| inclination: | 97.7792° |
| perigee height: | 579 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 285.4873° |
| argument of perigee: | 182.8795° |
| revolutions per day: | 14.85012026 |
| mean anomaly at epoch: | 177.2143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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