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 7714U 75023A 24358.20025202 .00000131 00000-0 69151-4 0 9992
2 7714 81.2034 37.4626 0029465 81.5055 278.9452 14.08369847871639
| Epoch (UTC): | 23 December 2024 04:48:21 |
| Eccentricity: | 0.0029465 |
| inclination: | 81.2034° |
| perigee height: | 843 km |
| apogee height: | 886 km |
| right ascension of ascending node: | 37.4626° |
| argument of perigee: | 81.5055° |
| revolutions per day: | 14.08369847 |
| mean anomaly at epoch: | 278.9452° |
| orbit number at epoch: | 87163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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