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 21067.88612156 .00000650 00000-0 28439-4 0 9998
2 20580 28.4708 10.4745 0002839 63.6616 334.5594 15.09576613495887
Epoch (UTC): | 08 March 2021 21:16:00 |
Eccentricity: | 0.0002839 |
inclination: | 28.4708° |
perigee height: | 535 km |
apogee height: | 539 km |
right ascension of ascending node: | 10.4745° |
argument of perigee: | 63.6616° |
revolutions per day: | 15.09576613 |
mean anomaly at epoch: | 334.5594° |
orbit number at epoch: | 49588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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