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 25860U 99039A 25191.42246394 .00000420 00000-0 62752-4 0 9995
2 25860 97.9823 248.2765 0001818 78.5783 281.5632 14.79834597398555
| Epoch (UTC): | 10 July 2025 10:08:20 |
| Eccentricity: | 0.0001818 |
| inclination: | 97.9823° |
| perigee height: | 628 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 248.2765° |
| argument of perigee: | 78.5783° |
| revolutions per day: | 14.79834597 |
| mean anomaly at epoch: | 281.5632° |
| orbit number at epoch: | 39855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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