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 data is extracted from the following two-line orbital elements,
1 40931U 15052B 25151.18580782 .00001310 00000-0 87238-4 0 9990
2 40931 6.0001 24.1284 0012872 339.0660 20.8941 14.78806187523154
| Epoch (UTC): | 31 May 2025 04:27:33 |
| Eccentricity: | 0.0012872 |
| inclination: | 6.0001° |
| perigee height: | 624 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 24.1284° |
| argument of perigee: | 339.0660° |
| revolutions per day: | 14.78806187 |
| mean anomaly at epoch: | 20.8941° |
| orbit number at epoch: | 52315 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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