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 25136.52645524 .00008874 00000-0 88181-2 0 9990
2 59588 97.4812 137.5451 0050330 80.0478 280.6354 13.77737522 53136
| Epoch (UTC): | 16 May 2025 12:38:05 |
| Eccentricity: | 0.0050330 |
| inclination: | 97.4812° |
| perigee height: | 935 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 137.5451° |
| argument of perigee: | 80.0478° |
| revolutions per day: | 13.77737522 |
| mean anomaly at epoch: | 280.6354° |
| orbit number at epoch: | 5313 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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