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 25137.25268513 .00010846 00000-0 10765-1 0 9994
2 59588 97.4814 138.1188 0050429 80.2302 280.4545 13.77753755 53236
| Epoch (UTC): | 17 May 2025 06:03:51 |
| Eccentricity: | 0.0050429 |
| inclination: | 97.4814° |
| perigee height: | 935 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 138.1188° |
| argument of perigee: | 80.2302° |
| revolutions per day: | 13.77753755 |
| mean anomaly at epoch: | 280.4545° |
| orbit number at epoch: | 5323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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