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 14452U 83109A 24357.99069815 .00000279 00000-0 10510-3 0 9993
2 14452 81.1598 183.9968 0089571 334.8949 24.7888 14.27045444140517
| Epoch (UTC): | 22 December 2024 23:46:36 |
| Eccentricity: | 0.0089571 |
| inclination: | 81.1598° |
| perigee height: | 737 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 183.9968° |
| argument of perigee: | 334.8949° |
| revolutions per day: | 14.27045444 |
| mean anomaly at epoch: | 24.7888° |
| orbit number at epoch: | 14051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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