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 42724U 98067MD 18238.55288637 .32989438 12602-4 94761-3 0 9996
2 42724 51.6129 331.1144 0008406 301.9468 58.5777 16.44741502 71945
Epoch (UTC): | 26 August 2018 13:16:09 |
Eccentricity: | 0.0008406 |
inclination: | 51.6129° |
perigee height: | 148 km |
apogee height: | 159 km |
right ascension of ascending node: | 331.1144° |
argument of perigee: | 301.9468° |
revolutions per day: | 16.44741502 |
mean anomaly at epoch: | 58.5777° |
orbit number at epoch: | 7194 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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