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 59626U 24081B 24357.83938251 .00009798 00000-0 50644-3 0 9998
2 59626 97.5570 68.6789 0000897 168.0356 192.0899 15.16478515 35481
| Epoch (UTC): | 22 December 2024 20:08:42 |
| Eccentricity: | 0.0000897 |
| inclination: | 97.5570° |
| perigee height: | 516 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 68.6789° |
| argument of perigee: | 168.0356° |
| revolutions per day: | 15.16478515 |
| mean anomaly at epoch: | 192.0899° |
| orbit number at epoch: | 3548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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