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 44475U 19049A 22026.56380734 .00000164 00000-0 00000-0 0 9996
2 44475 0.0926 267.5182 0000626 58.6848 33.7773 1.00275539 9132
| Epoch (UTC): | 26 January 2022 13:31:52 |
| Eccentricity: | 0.0000626 |
| inclination: | 0.0926° |
| perigee height: | 35782 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 267.5182° |
| argument of perigee: | 58.6848° |
| revolutions per day: | 1.00275539 |
| mean anomaly at epoch: | 33.7773° |
| orbit number at epoch: | 913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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