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 27386U 02009A 21025.53798177 .00000033 00000-0 24298-4 0 9999
2 27386 98.1420 26.9475 0001179 87.6858 21.0982 14.38009973990537
Epoch (UTC): | 25 January 2021 12:54:41 |
Eccentricity: | 0.0001179 |
inclination: | 98.1420° |
perigee height: | 764 km |
apogee height: | 766 km |
right ascension of ascending node: | 26.9475° |
argument of perigee: | 87.6858° |
revolutions per day: | 14.38009973 |
mean anomaly at epoch: | 21.0982° |
orbit number at epoch: | 99053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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