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 31114U 07010B 25191.57824710 .00000052 00000-0 42913-4 0 9990
2 31114 98.3823 312.1896 0057883 278.3987 81.0631 14.20135168945356
| Epoch (UTC): | 10 July 2025 13:52:40 |
| Eccentricity: | 0.0057883 |
| inclination: | 98.3823° |
| perigee height: | 783 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 312.1896° |
| argument of perigee: | 278.3987° |
| revolutions per day: | 14.20135168 |
| mean anomaly at epoch: | 81.0631° |
| orbit number at epoch: | 94535 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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