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 40940U 26145.32635654 +.00000000 +00000-0 +00000-0 0 00002
2 40940 0.0159 300.6662 0001841 115.5072 84.4903 1.00272592 08
| Epoch (UTC): | 25 May 2026 07:49:57 |
| Eccentricity: | 0.0001841 |
| inclination: | 0.0159° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 300.6662° |
| argument of perigee: | 115.5072° |
| revolutions per day: | 1.00272592 |
| mean anomaly at epoch: | 84.4903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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