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 24280.86909669 .00015358 00000-0 11736-2 0 9993
2 20682 63.2981 71.0244 0906319 70.9891 298.7037 13.55095908 19707
| Epoch (UTC): | 06 October 2024 20:51:29 |
| Eccentricity: | 0.0906319 |
| inclination: | 63.2981° |
| perigee height: | 380 km |
| apogee height: | 1727 km |
| right ascension of ascending node: | 71.0244° |
| argument of perigee: | 70.9891° |
| revolutions per day: | 13.55095908 |
| mean anomaly at epoch: | 298.7037° |
| orbit number at epoch: | 1970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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