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 36800U 10035F 21058.87030657 .00000551 00000-0 56202-4 0 9998
2 36800 98.1622 252.7011 0021845 192.3689 167.6997 14.94865841578783
Epoch (UTC): | 27 February 2021 20:53:14 |
Eccentricity: | 0.0021845 |
inclination: | 98.1622° |
perigee height: | 567 km |
apogee height: | 598 km |
right ascension of ascending node: | 252.7011° |
argument of perigee: | 192.3689° |
revolutions per day: | 14.94865841 |
mean anomaly at epoch: | 167.6997° |
orbit number at epoch: | 57878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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