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 19050.29851099 .00016717 00000-0 10270-3 0 9049
2 25544 51.6386 227.4344 0005643 40.2449 319.9120 15.53305359 36933
Epoch (UTC): | 19 February 2019 07:09:51 |
Eccentricity: | 0.0005643 |
inclination: | 51.6386° |
perigee height: | 403 km |
apogee height: | 411 km |
right ascension of ascending node: | 227.4344° |
argument of perigee: | 40.2449° |
revolutions per day: | 15.53305359 |
mean anomaly at epoch: | 319.9120° |
orbit number at epoch: | 3693 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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