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 25341.91481825 .00039592 00000-0 33983-1 0 9993
2 59588 97.2728 298.5977 0078026 349.1031 10.8437 13.85122195 81473
| Epoch (UTC): | 07 December 2025 21:57:20 |
| Eccentricity: | 0.0078026 |
| inclination: | 97.2728° |
| perigee height: | 888 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 298.5977° |
| argument of perigee: | 349.1031° |
| revolutions per day: | 13.85122195 |
| mean anomaly at epoch: | 10.8437° |
| orbit number at epoch: | 8147 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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