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 406U 61015EF 24357.62111490 .00000740 00000-0 89840-3 0 9991
2 406 66.7760 189.7807 0116635 37.8519 29.6887 13.68847479147491
| Epoch (UTC): | 22 December 2024 14:54:24 |
| Eccentricity: | 0.0116635 |
| inclination: | 66.7760° |
| perigee height: | 917 km |
| apogee height: | 1090 km |
| right ascension of ascending node: | 189.7807° |
| argument of perigee: | 37.8519° |
| revolutions per day: | 13.68847479 |
| mean anomaly at epoch: | 29.6887° |
| orbit number at epoch: | 14749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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