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 58200U 23168B 24357.61880967 .00007252 00000-0 42091-3 0 9996
2 58200 97.7958 13.5068 0070678 55.3034 305.4826 15.10322177 62907
| Epoch (UTC): | 22 December 2024 14:51:05 |
| Eccentricity: | 0.0070678 |
| inclination: | 97.7958° |
| perigee height: | 486 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 13.5068° |
| argument of perigee: | 55.3034° |
| revolutions per day: | 15.10322177 |
| mean anomaly at epoch: | 305.4826° |
| orbit number at epoch: | 6290 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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