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 39152U 13018C 21016.15675581 .00000221 00000-0 35241-4 0 9995
2 39152 97.8928 107.5308 0018059 112.3839 247.9289 14.80954390417263
Epoch (UTC): | 16 January 2021 03:45:43 |
Eccentricity: | 0.0018059 |
inclination: | 97.8928° |
perigee height: | 613 km |
apogee height: | 639 km |
right ascension of ascending node: | 107.5308° |
argument of perigee: | 112.3839° |
revolutions per day: | 14.80954390 |
mean anomaly at epoch: | 247.9289° |
orbit number at epoch: | 41726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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