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 27582U 01049NA 24357.83505326 .00014829 00000-0 12459-2 0 9998
2 27582 98.3830 16.0846 0037717 20.1199 340.1497 14.97862727211509
| Epoch (UTC): | 22 December 2024 20:02:28 |
| Eccentricity: | 0.0037717 |
| inclination: | 98.3830° |
| perigee height: | 547 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 16.0846° |
| argument of perigee: | 20.1199° |
| revolutions per day: | 14.97862727 |
| mean anomaly at epoch: | 340.1497° |
| orbit number at epoch: | 21150 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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