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 54550U 22151LA 24285.47298286 .00008879 00000-0 30576-2 0 9992
2 54550 98.7266 306.8593 0067078 329.3249 30.4021 14.34898722 99920
| Epoch (UTC): | 11 October 2024 11:21:05 |
| Eccentricity: | 0.0067078 |
| inclination: | 98.7266° |
| perigee height: | 727 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 306.8593° |
| argument of perigee: | 329.3249° |
| revolutions per day: | 14.34898722 |
| mean anomaly at epoch: | 30.4021° |
| orbit number at epoch: | 9992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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