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 16263U 85108B 24285.60312128 .00002496 00000-0 29191-3 0 9990
2 16263 82.5005 125.0626 0019496 174.5598 244.9327 14.84607625 79628
| Epoch (UTC): | 11 October 2024 14:28:29 |
| Eccentricity: | 0.0019496 |
| inclination: | 82.5005° |
| perigee height: | 601 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 125.0626° |
| argument of perigee: | 174.5598° |
| revolutions per day: | 14.84607625 |
| mean anomaly at epoch: | 244.9327° |
| orbit number at epoch: | 7962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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