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 05918U 72022B 21055.54506607 -.00000013 00000-0 -15535-4 0 9991
2 05918 81.2356 101.5001 0059559 137.3087 223.2733 14.05879851507181
Epoch (UTC): | 24 February 2021 13:04:53 |
Eccentricity: | 0.0059559 |
inclination: | 81.2356° |
perigee height: | 830 km |
apogee height: | 916 km |
right ascension of ascending node: | 101.5001° |
argument of perigee: | 137.3087° |
revolutions per day: | 14.05879851 |
mean anomaly at epoch: | 223.2733° |
orbit number at epoch: | 50718 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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