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 40107U 26107.03178818 +.00000000 +00000-0 +00000-0 0 00007
2 40107 0.0174 230.8081 0001290 160.0088 291.1185 1.00268577 06
| Epoch (UTC): | 17 April 2026 00:45:46 |
| Eccentricity: | 0.0001290 |
| inclination: | 0.0174° |
| perigee height: | 35782 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 230.8081° |
| argument of perigee: | 160.0088° |
| revolutions per day: | 1.00268577 |
| mean anomaly at epoch: | 291.1185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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