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 45117U 19071G 22179.49406432 .00019965 00000-0 37350-3 0 9990
2 45117 51.6378 359.8653 0008452 210.6256 149.4239 15.48670196135143
Epoch (UTC): | 28 June 2022 11:51:27 |
Eccentricity: | 0.0008452 |
inclination: | 51.6378° |
perigee height: | 415 km |
apogee height: | 426 km |
right ascension of ascending node: | 359.8653° |
argument of perigee: | 210.6256° |
revolutions per day: | 15.48670196 |
mean anomaly at epoch: | 149.4239° |
orbit number at epoch: | 13514 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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