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 20508U 90017A 25133.78539843 .00000071 00000-0 58510-4 0 9994
2 20508 82.9584 9.0856 0045306 112.6069 317.8239 13.74508835765515
| Epoch (UTC): | 13 May 2025 18:50:58 |
| Eccentricity: | 0.0045306 |
| inclination: | 82.9584° |
| perigee height: | 950 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 9.0856° |
| argument of perigee: | 112.6069° |
| revolutions per day: | 13.74508835 |
| mean anomaly at epoch: | 317.8239° |
| orbit number at epoch: | 76551 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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