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 20441U 90005F 21016.14783374 .00000010 00000-0 20481-4 0 9992
2 20441 98.7462 334.2616 0010376 260.4773 110.4479 14.32859141618931
Epoch (UTC): | 16 January 2021 03:32:52 |
Eccentricity: | 0.0010376 |
inclination: | 98.7462° |
perigee height: | 775 km |
apogee height: | 789 km |
right ascension of ascending node: | 334.2616° |
argument of perigee: | 260.4773° |
revolutions per day: | 14.32859141 |
mean anomaly at epoch: | 110.4479° |
orbit number at epoch: | 61893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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