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 19048.56139548 .00016717 00000-0 10270-3 0 9022
2 25544 51.6355 236.0800 0005585 35.0639 325.0880 15.53263123 36663
Epoch (UTC): | 17 February 2019 13:28:24 |
Eccentricity: | 0.0005585 |
inclination: | 51.6355° |
perigee height: | 403 km |
apogee height: | 411 km |
right ascension of ascending node: | 236.0800° |
argument of perigee: | 35.0639° |
revolutions per day: | 15.53263123 |
mean anomaly at epoch: | 325.0880° |
orbit number at epoch: | 3666 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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