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 20442U 90005G 23079.44020895 .00000358 00000-0 14706-3 0 9996
2 20442 98.8353 54.1041 0012868 79.8916 280.3718 14.33201827732697
| Epoch (UTC): | 20 March 2023 10:33:54 |
| Eccentricity: | 0.0012868 |
| inclination: | 98.8353° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 54.1041° |
| argument of perigee: | 79.8916° |
| revolutions per day: | 14.33201827 |
| mean anomaly at epoch: | 280.3718° |
| orbit number at epoch: | 73269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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