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 14699U 84013A 24358.02209637 .00009231 00000-0 47222-3 0 9991
2 14699 82.5471 184.3866 0018387 27.4508 332.7692 15.16359713226662
| Epoch (UTC): | 23 December 2024 00:31:49 |
| Eccentricity: | 0.0018387 |
| inclination: | 82.5471° |
| perigee height: | 504 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 184.3866° |
| argument of perigee: | 27.4508° |
| revolutions per day: | 15.16359713 |
| mean anomaly at epoch: | 332.7692° |
| orbit number at epoch: | 22666 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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