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 23090.37064917 .00000346 00000-0 15011-3 0 9994
2 22826 98.8462 131.8356 0007874 282.5057 77.5244 14.30631876539680
| Epoch (UTC): | 31 March 2023 08:53:44 |
| Eccentricity: | 0.0007874 |
| inclination: | 98.8462° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 131.8356° |
| argument of perigee: | 282.5057° |
| revolutions per day: | 14.30631876 |
| mean anomaly at epoch: | 77.5244° |
| orbit number at epoch: | 53968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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