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 25140.52061743 .00007762 00000-0 77054-2 0 9992
2 59588 97.4821 140.6994 0051043 81.2479 279.4453 13.77818579 53687
| Epoch (UTC): | 20 May 2025 12:29:41 |
| Eccentricity: | 0.0051043 |
| inclination: | 97.4821° |
| perigee height: | 934 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 140.6994° |
| argument of perigee: | 81.2479° |
| revolutions per day: | 13.77818579 |
| mean anomaly at epoch: | 279.4453° |
| orbit number at epoch: | 5368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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