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 25198.20581440 .00002481 00000-0 25645-3 0 9991
2 58909 50.0042 110.8313 0006771 318.2650 41.7775 14.93456165 79121
| Epoch (UTC): | 17 July 2025 04:56:22 |
| Eccentricity: | 0.0006771 |
| inclination: | 50.0042° |
| perigee height: | 582 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 110.8313° |
| argument of perigee: | 318.2650° |
| revolutions per day: | 14.93456165 |
| mean anomaly at epoch: | 41.7775° |
| orbit number at epoch: | 7912 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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