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 40921U 15050B 25012.86066236 .00000060 00000-0 35765-3 0 9999
2 40921 82.4859 42.2931 0015039 80.5645 279.7133 12.42888220422200
| Epoch (UTC): | 12 January 2025 20:39:21 |
| Eccentricity: | 0.0015039 |
| inclination: | 82.4859° |
| perigee height: | 1482 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 42.2931° |
| argument of perigee: | 80.5645° |
| revolutions per day: | 12.42888220 |
| mean anomaly at epoch: | 279.7133° |
| orbit number at epoch: | 42220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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