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 20104U 89050B 21055.53101356 -.00000053 00000-0 -68611-4 0 9992
2 20104 82.9524 251.0459 0043841 9.9456 350.2559 13.77325140589990
Epoch (UTC): | 24 February 2021 12:44:39 |
Eccentricity: | 0.0043841 |
inclination: | 82.9524° |
perigee height: | 941 km |
apogee height: | 1005 km |
right ascension of ascending node: | 251.0459° |
argument of perigee: | 9.9456° |
revolutions per day: | 13.77325140 |
mean anomaly at epoch: | 350.2559° |
orbit number at epoch: | 58999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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