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 13553U 82092B 22140.38538098 .00000486 00000-0 54827-4 0 9999
2 13553 82.5693 358.4802 0020266 218.6185 314.5936 14.84399582122682
Epoch (UTC): | 20 May 2022 09:14:56 |
Eccentricity: | 0.0020266 |
inclination: | 82.5693° |
perigee height: | 601 km |
apogee height: | 629 km |
right ascension of ascending node: | 358.4802° |
argument of perigee: | 218.6185° |
revolutions per day: | 14.84399582 |
mean anomaly at epoch: | 314.5936° |
orbit number at epoch: | 12268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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