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 25194.60947158 .00000363 00000-0 53431-4 0 9995
2 25861 98.0343 248.5559 0013892 316.7321 43.2799 14.81310996401466
Epoch (UTC): | 13 July 2025 14:37:38 |
Eccentricity: | 0.0013892 |
inclination: | 98.0343° |
perigee height: | 615 km |
apogee height: | 635 km |
right ascension of ascending node: | 248.5559° |
argument of perigee: | 316.7321° |
revolutions per day: | 14.81310996 |
mean anomaly at epoch: | 43.2799° |
orbit number at epoch: | 40146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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