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 21025.69615413 .00016717 00000-0 10270-3 0 9114
2 25544 51.6459 327.5036 0002381 294.4318 65.6583 15.48912524 26500
Epoch (UTC): | 25 January 2021 16:42:27 |
Eccentricity: | 0.0002381 |
inclination: | 51.6459° |
perigee height: | 418 km |
apogee height: | 421 km |
right ascension of ascending node: | 327.5036° |
argument of perigee: | 294.4318° |
revolutions per day: | 15.48912524 |
mean anomaly at epoch: | 65.6583° |
orbit number at epoch: | 2650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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