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 16383U 82055X 24262.82035591 .00000862 00000-0 97032-3 0 9990
2 16383 65.8300 54.5241 0053586 305.0151 161.9036 13.75357855947575
| Epoch (UTC): | 18 September 2024 19:41:18 |
| Eccentricity: | 0.0053586 |
| inclination: | 65.8300° |
| perigee height: | 941 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 54.5241° |
| argument of perigee: | 305.0151° |
| revolutions per day: | 13.75357855 |
| mean anomaly at epoch: | 161.9036° |
| orbit number at epoch: | 94757 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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