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 23151.81675333 .00000012 00000-0 30721-4 0 9998
2 22566 71.0068 182.0716 0008320 57.6459 302.5468 14.15067738558872
| Epoch (UTC): | 31 May 2023 19:36:07 |
| Eccentricity: | 0.0008320 |
| inclination: | 71.0068° |
| perigee height: | 836 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 182.0716° |
| argument of perigee: | 57.6459° |
| revolutions per day: | 14.15067738 |
| mean anomaly at epoch: | 302.5468° |
| orbit number at epoch: | 55887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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