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 00022U 59009A 21059.86259745 .00000179 00000-0 36354-4 0 9992
2 00022 50.2851 338.7487 0138794 158.5725 202.1110 14.95419149508739
Epoch (UTC): | 28 February 2021 20:42:08 |
Eccentricity: | 0.0138794 |
inclination: | 50.2851° |
perigee height: | 484 km |
apogee height: | 677 km |
right ascension of ascending node: | 338.7487° |
argument of perigee: | 158.5725° |
revolutions per day: | 14.95419149 |
mean anomaly at epoch: | 202.1110° |
orbit number at epoch: | 50873 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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