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 59588U 24077B 25348.92038268 .00022676 00000-0 19362-1 0 9990
2 59588 97.2653 304.0397 0077096 333.1816 26.5368 13.85612488 82443
| Epoch (UTC): | 14 December 2025 22:05:21 |
| Eccentricity: | 0.0077096 |
| inclination: | 97.2653° |
| perigee height: | 887 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 304.0397° |
| argument of perigee: | 333.1816° |
| revolutions per day: | 13.85612488 |
| mean anomaly at epoch: | 26.5368° |
| orbit number at epoch: | 8244 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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