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 25682U 99020A 25341.98431605 .00000867 00000-0 17514-3 0 9996
2 25682 97.8591 349.4162 0001313 75.3854 344.7225 14.63686502417878
| Epoch (UTC): | 07 December 2025 23:37:24 |
| Eccentricity: | 0.0001313 |
| inclination: | 97.8591° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 349.4162° |
| argument of perigee: | 75.3854° |
| revolutions per day: | 14.63686502 |
| mean anomaly at epoch: | 344.7225° |
| orbit number at epoch: | 41787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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