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 25117.49629443 .00015539 00000-0 15515-1 0 9993
2 59588 97.4810 122.5250 0051898 79.5075 281.1923 13.77286233 50516
| Epoch (UTC): | 27 April 2025 11:54:39 |
| Eccentricity: | 0.0051898 |
| inclination: | 97.4810° |
| perigee height: | 935 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 122.5250° |
| argument of perigee: | 79.5075° |
| revolutions per day: | 13.77286233 |
| mean anomaly at epoch: | 281.1923° |
| orbit number at epoch: | 5051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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