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 22221.68207723 -.00000285 00000-0 -12248-3 0 9991
2 22566 71.0072 81.6501 0009504 166.7646 193.3728 14.15006380517122
| Epoch (UTC): | 09 August 2022 16:22:11 |
| Eccentricity: | 0.0009504 |
| inclination: | 71.0072° |
| perigee height: | 835 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 81.6501° |
| argument of perigee: | 166.7646° |
| revolutions per day: | 14.15006380 |
| mean anomaly at epoch: | 193.3728° |
| orbit number at epoch: | 51712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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