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 25193.44410338 .00000087 00000-0 50133-4 0 9997
2 22826 98.7299 255.0469 0008968 8.5540 351.5794 14.31222337658719
| Epoch (UTC): | 12 July 2025 10:39:30 |
| Eccentricity: | 0.0008968 |
| inclination: | 98.7299° |
| perigee height: | 781 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 255.0469° |
| argument of perigee: | 8.5540° |
| revolutions per day: | 14.31222337 |
| mean anomaly at epoch: | 351.5794° |
| orbit number at epoch: | 65871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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