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 32156U 99025CTA 22171.96639091 .00000488 00000-0 20804-3 0 9995
2 32156 99.2973 239.8642 0088296 110.0960 250.9748 14.27877596466638
| Epoch (UTC): | 20 June 2022 23:11:36 |
| Eccentricity: | 0.0088296 |
| inclination: | 99.2973° |
| perigee height: | 735 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 239.8642° |
| argument of perigee: | 110.0960° |
| revolutions per day: | 14.27877596 |
| mean anomaly at epoch: | 250.9748° |
| orbit number at epoch: | 46663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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