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 22826U 93061D 25107.73339971 .00000284 00000-0 12469-3 0 9995
2 22826 98.7359 168.8931 0007850 249.0017 111.0326 14.31186968646458
Epoch (UTC): | 17 April 2025 17:36:05 |
Eccentricity: | 0.0007850 |
inclination: | 98.7359° |
perigee height: | 782 km |
apogee height: | 793 km |
right ascension of ascending node: | 168.8931° |
argument of perigee: | 249.0017° |
revolutions per day: | 14.31186968 |
mean anomaly at epoch: | 111.0326° |
orbit number at epoch: | 64645 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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