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 25343.64840030 .00032812 00000-0 28136-1 0 9994
2 59588 97.2710 299.9445 0077938 345.3697 14.5208 13.85240551 81717
| Epoch (UTC): | 09 December 2025 15:33:41 |
| Eccentricity: | 0.0077938 |
| inclination: | 97.2710° |
| perigee height: | 888 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 299.9445° |
| argument of perigee: | 345.3697° |
| revolutions per day: | 13.85240551 |
| mean anomaly at epoch: | 14.5208° |
| orbit number at epoch: | 8171 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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