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 28522U 05002B 23152.42702290 -.00000015 00000-0 -25279-4 0 9992
2 28522 82.9445 145.9778 0045806 169.9064 190.3031 13.89717965931154
| Epoch (UTC): | 01 June 2023 10:14:54 |
| Eccentricity: | 0.0045806 |
| inclination: | 82.9445° |
| perigee height: | 896 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 145.9778° |
| argument of perigee: | 169.9064° |
| revolutions per day: | 13.89717965 |
| mean anomaly at epoch: | 190.3031° |
| orbit number at epoch: | 93115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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