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 22566U 93016B 23147.43402989 .00000195 00000-0 12501-3 0 9993
2 22566 71.0072 191.2726 0008307 66.7367 293.4629 14.15066465558260
| Epoch (UTC): | 27 May 2023 10:25:00 |
| Eccentricity: | 0.0008307 |
| inclination: | 71.0072° |
| perigee height: | 836 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 191.2726° |
| argument of perigee: | 66.7367° |
| revolutions per day: | 14.15066465 |
| mean anomaly at epoch: | 293.4629° |
| orbit number at epoch: | 55826 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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