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 05024U 70025HY 24285.64929884 .00012591 00000-0 54705-2 0 9997
2 05024 99.8063 170.7936 0087744 46.9188 313.9287 14.22203147784689
| Epoch (UTC): | 11 October 2024 15:34:59 |
| Eccentricity: | 0.0087744 |
| inclination: | 99.8063° |
| perigee height: | 755 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 170.7936° |
| argument of perigee: | 46.9188° |
| revolutions per day: | 14.22203147 |
| mean anomaly at epoch: | 313.9287° |
| orbit number at epoch: | 78468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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