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 25080.60741605 .00000432 00000-0 18057-3 0 9996
2 22826 98.7410 141.6091 0008360 338.3573 21.7255 14.31163128642578
| Epoch (UTC): | 21 March 2025 14:34:40 |
| Eccentricity: | 0.0008360 |
| inclination: | 98.7410° |
| perigee height: | 782 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 141.6091° |
| argument of perigee: | 338.3573° |
| revolutions per day: | 14.31163128 |
| mean anomaly at epoch: | 21.7255° |
| orbit number at epoch: | 64257 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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