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 19344.44856133 .00016717 00000-0 10270-3 0 9103
2 25544 51.6422 207.4676 0007378 17.4899 342.6504 15.50104272 2594
Epoch (UTC): | 10 December 2019 10:45:55 |
Eccentricity: | 0.0007378 |
inclination: | 51.6422° |
perigee height: | 411 km |
apogee height: | 421 km |
right ascension of ascending node: | 207.4676° |
argument of perigee: | 17.4899° |
revolutions per day: | 15.50104272 |
mean anomaly at epoch: | 342.6504° |
orbit number at epoch: | 259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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