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 5682U 71110E 25322.49110477 .00000002 00000-0 55415-4 0 9994
2 5682 69.9894 80.9261 0005468 67.1031 293.0640 13.74632261316228
| Epoch (UTC): | 18 November 2025 11:47:11 |
| Eccentricity: | 0.0005468 |
| inclination: | 69.9894° |
| perigee height: | 979 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 80.9261° |
| argument of perigee: | 67.1031° |
| revolutions per day: | 13.74632261 |
| mean anomaly at epoch: | 293.0640° |
| orbit number at epoch: | 31622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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