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 23087.92278906 .00000285 00000-0 12660-3 0 9995
2 22826 98.8466 129.3456 0007913 290.5844 69.4488 14.30629886539334
| Epoch (UTC): | 28 March 2023 22:08:48 |
| Eccentricity: | 0.0007913 |
| inclination: | 98.8466° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 129.3456° |
| argument of perigee: | 290.5844° |
| revolutions per day: | 14.30629886 |
| mean anomaly at epoch: | 69.4488° |
| orbit number at epoch: | 53933 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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