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 20478U 90013A 21103.01892577 .00000219 00000-0 19581-3 0 9999
2 20478 99.4305 111.6746 0004510 281.0645 79.0008 13.95527859508422
Epoch (UTC): | 13 April 2021 00:27:15 |
Eccentricity: | 0.0004510 |
inclination: | 99.4305° |
perigee height: | 906 km |
apogee height: | 912 km |
right ascension of ascending node: | 111.6746° |
argument of perigee: | 281.0645° |
revolutions per day: | 13.95527859 |
mean anomaly at epoch: | 79.0008° |
orbit number at epoch: | 50842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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