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 25197.71671052 .00000333 00000-0 49582-4 0 9996
2 25861 98.0341 251.6711 0013732 305.9170 54.0767 14.81313498401920
| Epoch (UTC): | 16 July 2025 17:12:03 |
| Eccentricity: | 0.0013732 |
| inclination: | 98.0341° |
| perigee height: | 615 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 251.6711° |
| argument of perigee: | 305.9170° |
| revolutions per day: | 14.81313498 |
| mean anomaly at epoch: | 54.0767° |
| orbit number at epoch: | 40192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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