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 19345.48007397 .00016717 00000-0 10270-3 0 9119
2 25544 51.6421 202.3571 0007380 21.8987 338.2478 15.50089789 2755
Epoch (UTC): | 11 December 2019 11:31:18 |
Eccentricity: | 0.0007380 |
inclination: | 51.6421° |
perigee height: | 411 km |
apogee height: | 421 km |
right ascension of ascending node: | 202.3571° |
argument of perigee: | 21.8987° |
revolutions per day: | 15.50089789 |
mean anomaly at epoch: | 338.2478° |
orbit number at epoch: | 275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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