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 25861U 99039B 25194.13663049 .00000355 00000-0 52402-4 0 9995
2 25861 98.0344 248.0818 0013925 318.3334 41.6817 14.81310527401529
| Epoch (UTC): | 13 July 2025 03:16:44 |
| Eccentricity: | 0.0013925 |
| inclination: | 98.0344° |
| perigee height: | 615 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 248.0818° |
| argument of perigee: | 318.3334° |
| revolutions per day: | 14.81310527 |
| mean anomaly at epoch: | 41.6817° |
| orbit number at epoch: | 40152 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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