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 39762U 14028B 18113.68989980 .00000048 00000-0 27753-3 0 9992
2 39762 82.4526 173.6968 0021799 77.7122 282.6400 12.42885737177824
Epoch (UTC): | 23 April 2018 16:33:27 |
Eccentricity: | 0.0021799 |
inclination: | 82.4526° |
perigee height: | 1477 km |
apogee height: | 1511 km |
right ascension of ascending node: | 173.6968° |
argument of perigee: | 77.7122° |
revolutions per day: | 12.42885737 |
mean anomaly at epoch: | 282.6400° |
orbit number at epoch: | 17782 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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