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 23341.09055092 .00000170 00000-0 82255-4 0 9996
2 22826 98.8137 26.4384 0007918 268.5497 91.4778 14.30762667575286
| Epoch (UTC): | 07 December 2023 02:10:23 |
| Eccentricity: | 0.0007918 |
| inclination: | 98.8137° |
| perigee height: | 783 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 26.4384° |
| argument of perigee: | 268.5497° |
| revolutions per day: | 14.30762667 |
| mean anomaly at epoch: | 91.4778° |
| orbit number at epoch: | 57528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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