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 25338.80840008 .00024642 00000-0 21306-1 0 9995
2 59588 97.2747 296.1857 0077263 354.7889 5.2460 13.84865597 81046
| Epoch (UTC): | 04 December 2025 19:24:05 |
| Eccentricity: | 0.0077263 |
| inclination: | 97.2747° |
| perigee height: | 890 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 296.1857° |
| argument of perigee: | 354.7889° |
| revolutions per day: | 13.84865597 |
| mean anomaly at epoch: | 5.2460° |
| orbit number at epoch: | 8104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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