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 00020U 59007A 21023.90411740 .00000102 00000-0 41610-4 0 9996
2 00020 33.3454 116.6611 1665994 356.1804 2.7336 11.55793762256117
Epoch (UTC): | 23 January 2021 21:41:55 |
Eccentricity: | 0.1665994 |
inclination: | 33.3454° |
perigee height: | 508 km |
apogee height: | 3261 km |
right ascension of ascending node: | 116.6611° |
argument of perigee: | 356.1804° |
revolutions per day: | 11.55793762 |
mean anomaly at epoch: | 2.7336° |
orbit number at epoch: | 25611 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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