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 20U 59007A 21057.86390845 .00000107 00000-0 36091-4 0 9992
2 20 33.3473 355.6511 1665821 176.4029 185.0397 11.55800484260075
Epoch (UTC): | 26 February 2021 20:44:01 |
Eccentricity: | 0.1665821 |
inclination: | 33.3473° |
perigee height: | 508 km |
apogee height: | 3261 km |
right ascension of ascending node: | 355.6511° |
argument of perigee: | 176.4029° |
revolutions per day: | 11.55800484 |
mean anomaly at epoch: | 185.0397° |
orbit number at epoch: | 26007 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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