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 19346.78167135 .00000361 00000-0 10958-4 0 9992
2 20580 28.4687 120.8672 0002536 229.4404 278.7262 15.09310911427679
Epoch (UTC): | 12 December 2019 18:45:36 |
Eccentricity: | 0.0002536 |
inclination: | 28.4687° |
perigee height: | 536 km |
apogee height: | 540 km |
right ascension of ascending node: | 120.8672° |
argument of perigee: | 229.4404° |
revolutions per day: | 15.09310911 |
mean anomaly at epoch: | 278.7262° |
orbit number at epoch: | 42767 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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