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 24279.15237221 .00000195 00000-0 12506-3 0 9999
2 22566 71.0072 228.3688 0009183 22.1882 337.9636 14.15172486628531
| Epoch (UTC): | 05 October 2024 03:39:24 |
| Eccentricity: | 0.0009183 |
| inclination: | 71.0072° |
| perigee height: | 835 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 228.3688° |
| argument of perigee: | 22.1882° |
| revolutions per day: | 14.15172486 |
| mean anomaly at epoch: | 337.9636° |
| orbit number at epoch: | 62853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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