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 58909U 24023E 24358.14395837 .00008777 00000-0 85271-3 0 9999
2 58909 50.0058 359.1801 0006128 335.1836 24.8811 14.93200076 48349
| Epoch (UTC): | 23 December 2024 03:27:18 |
| Eccentricity: | 0.0006128 |
| inclination: | 50.0058° |
| perigee height: | 584 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 359.1801° |
| argument of perigee: | 335.1836° |
| revolutions per day: | 14.93200076 |
| mean anomaly at epoch: | 24.8811° |
| orbit number at epoch: | 4834 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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