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 21102.53990745 .00000731 00000-0 21496-4 0 9995
2 25544 51.6439 307.4244 0002838 218.7371 162.3034 15.48882554278426
Epoch (UTC): | 12 April 2021 12:57:28 |
Eccentricity: | 0.0002838 |
inclination: | 51.6439° |
perigee height: | 418 km |
apogee height: | 422 km |
right ascension of ascending node: | 307.4244° |
argument of perigee: | 218.7371° |
revolutions per day: | 15.48882554 |
mean anomaly at epoch: | 162.3034° |
orbit number at epoch: | 27842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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