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 23332.55877681 .00000348 00000-0 15042-3 0 9999
2 22826 98.8148 17.7914 0007982 296.6069 63.4295 14.30756769574062
| Epoch (UTC): | 28 November 2023 13:24:38 |
| Eccentricity: | 0.0007982 |
| inclination: | 98.8148° |
| perigee height: | 783 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 17.7914° |
| argument of perigee: | 296.6069° |
| revolutions per day: | 14.30756769 |
| mean anomaly at epoch: | 63.4295° |
| orbit number at epoch: | 57406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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