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 22566U 93016B 21101.86834555 .00000209 00000-0 13255-3 0 9999
2 22566 71.0107 19.3445 0010340 183.6596 176.4453 14.14973284448549
Epoch (UTC): | 11 April 2021 20:50:25 |
Eccentricity: | 0.0010340 |
inclination: | 71.0107° |
perigee height: | 835 km |
apogee height: | 850 km |
right ascension of ascending node: | 19.3445° |
argument of perigee: | 183.6596° |
revolutions per day: | 14.14973284 |
mean anomaly at epoch: | 176.4453° |
orbit number at epoch: | 44854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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