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 25544U 98067A 19052.29296672 .00016717 00000-0 10270-3 0 9030
2 25544 51.6398 217.5041 0005851 45.9800 314.1834 15.53320976 37240
Epoch (UTC): | 21 February 2019 07:01:52 |
Eccentricity: | 0.0005851 |
inclination: | 51.6398° |
perigee height: | 403 km |
apogee height: | 411 km |
right ascension of ascending node: | 217.5041° |
argument of perigee: | 45.9800° |
revolutions per day: | 15.53320976 |
mean anomaly at epoch: | 314.1834° |
orbit number at epoch: | 3724 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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