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 19053.90068709 .00000419 00000-0 14574-4 0 9990
2 20580 28.4685 257.5769 0002614 321.1491 167.9724 15.09176762383380
Epoch (UTC): | 22 February 2019 21:36:59 |
Eccentricity: | 0.0002614 |
inclination: | 28.4685° |
perigee height: | 537 km |
apogee height: | 540 km |
right ascension of ascending node: | 257.5769° |
argument of perigee: | 321.1491° |
revolutions per day: | 15.09176762 |
mean anomaly at epoch: | 167.9724° |
orbit number at epoch: | 38338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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