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 19348.76611410 +.00000372 +00000-0 +11655-4 0 9999
2 20580 028.4691 107.7434 0002497 252.7493 259.2987 15.09311748427887
Epoch (UTC): | 14 December 2019 18:23:12 |
Eccentricity: | 0.0002497 |
inclination: | 28.4691° |
perigee height: | 536 km |
apogee height: | 540 km |
right ascension of ascending node: | 107.7434° |
argument of perigee: | 252.7493° |
revolutions per day: | 15.09311748 |
mean anomaly at epoch: | 259.2987° |
orbit number at epoch: | 42788 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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