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 23080.85894953 .00000223 00000-0 10299-3 0 9994
2 22826 98.8480 122.1595 0008102 313.7155 46.3355 14.30624611538077
| Epoch (UTC): | 21 March 2023 20:36:53 |
| Eccentricity: | 0.0008102 |
| inclination: | 98.8480° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 122.1595° |
| argument of perigee: | 313.7155° |
| revolutions per day: | 14.30624611 |
| mean anomaly at epoch: | 46.3355° |
| orbit number at epoch: | 53807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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