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 5732U 71120B 24358.13399376 .00000147 00000-0 81133-4 0 9993
2 5732 81.2520 350.2768 0049839 241.2195 118.3964 14.06306295724804
| Epoch (UTC): | 23 December 2024 03:12:57 |
| Eccentricity: | 0.0049839 |
| inclination: | 81.2520° |
| perigee height: | 836 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 350.2768° |
| argument of perigee: | 241.2195° |
| revolutions per day: | 14.06306295 |
| mean anomaly at epoch: | 118.3964° |
| orbit number at epoch: | 72480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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