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 21529U 91045C 24278.09904838 .00005438 00000-0 17910-2 0 9992
2 21529 89.5834 328.4774 0054060 64.7849 295.8942 14.37253833736550
| Epoch (UTC): | 04 October 2024 02:22:37 |
| Eccentricity: | 0.0054060 |
| inclination: | 89.5834° |
| perigee height: | 729 km |
| apogee height: | 806 km |
| right ascension of ascending node: | 328.4774° |
| argument of perigee: | 64.7849° |
| revolutions per day: | 14.37253833 |
| mean anomaly at epoch: | 295.8942° |
| orbit number at epoch: | 73655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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