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 24357.79068332 .00011574 00000-0 86450-3 0 9995
2 20682 63.2956 225.7790 0901581 72.4501 297.2903 13.56768127 30131
| Epoch (UTC): | 22 December 2024 18:58:35 |
| Eccentricity: | 0.0901581 |
| inclination: | 63.2956° |
| perigee height: | 378 km |
| apogee height: | 1717 km |
| right ascension of ascending node: | 225.7790° |
| argument of perigee: | 72.4501° |
| revolutions per day: | 13.56768127 |
| mean anomaly at epoch: | 297.2903° |
| orbit number at epoch: | 3013 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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