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 22227.00885391 .00005694 00000-0 10700-3 0 9994
2 25544 51.6425 45.1868 0005588 122.1015 19.6650 15.50180483354302
Epoch (UTC): | 15 August 2022 00:12:44 |
Eccentricity: | 0.0005588 |
inclination: | 51.6425° |
perigee height: | 412 km |
apogee height: | 420 km |
right ascension of ascending node: | 45.1868° |
argument of perigee: | 122.1015° |
revolutions per day: | 15.50180483 |
mean anomaly at epoch: | 19.6650° |
orbit number at epoch: | 35430 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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