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 20466U 90010B 22230.01589536 .00000265 00000-0 30693-4 0 9992
2 20466 82.5015 45.9175 0018984 255.9087 104.0017 14.81573559756984
| Epoch (UTC): | 18 August 2022 00:22:53 |
| Eccentricity: | 0.0018984 |
| inclination: | 82.5015° |
| perigee height: | 611 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 45.9175° |
| argument of perigee: | 255.9087° |
| revolutions per day: | 14.81573559 |
| mean anomaly at epoch: | 104.0017° |
| orbit number at epoch: | 75698 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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