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 25171.44900970 .00009770 00000-0 95111-2 0 9996
2 59588 97.4699 165.0929 0067335 78.9073 281.9647 13.78483447 57942
| Epoch (UTC): | 20 June 2025 10:46:34 |
| Eccentricity: | 0.0067335 |
| inclination: | 97.4699° |
| perigee height: | 920 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 165.0929° |
| argument of perigee: | 78.9073° |
| revolutions per day: | 13.78483447 |
| mean anomaly at epoch: | 281.9647° |
| orbit number at epoch: | 5794 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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