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 20682U 90050B 25196.81255148 .00007404 00000-0 52034-3 0 9991
2 20682 63.2958 36.0786 0891237 76.4333 293.4291 13.60704072 57999
| Epoch (UTC): | 15 July 2025 19:30:04 |
| Eccentricity: | 0.0891237 |
| inclination: | 63.2958° |
| perigee height: | 372 km |
| apogee height: | 1693 km |
| right ascension of ascending node: | 36.0786° |
| argument of perigee: | 76.4333° |
| revolutions per day: | 13.60704072 |
| mean anomaly at epoch: | 293.4291° |
| orbit number at epoch: | 5799 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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