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 20580U 90037B 18110.21178775 .00000468 00000-0 17681-4 0 9998
2 20580 28.4687 138.3511 0002490 233.6785 19.9491 15.09020052336709
Epoch (UTC): | 20 April 2018 05:04:58 |
Eccentricity: | 0.0002490 |
inclination: | 28.4687° |
perigee height: | 537 km |
apogee height: | 541 km |
right ascension of ascending node: | 138.3511° |
argument of perigee: | 233.6785° |
revolutions per day: | 15.09020052 |
mean anomaly at epoch: | 19.9491° |
orbit number at epoch: | 33670 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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