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 20625U 90046B 25189.45308911 -.00000117 00000-0 -35680-4 0 9997
2 20625 71.0002 90.8348 0016033 310.0369 49.9346 14.14971747813848
Epoch (UTC): | 08 July 2025 10:52:26 |
Eccentricity: | 0.0016033 |
inclination: | 71.0002° |
perigee height: | 831 km |
apogee height: | 854 km |
right ascension of ascending node: | 90.8348° |
argument of perigee: | 310.0369° |
revolutions per day: | 14.14971747 |
mean anomaly at epoch: | 49.9346° |
orbit number at epoch: | 81384 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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