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 21938U 92020B 22221.78228633 .00000013 00000-0 -16184-5 0 9994
2 21938 82.9281 44.9935 0028951 350.5638 20.1858 13.75303725521349
Epoch (UTC): | 09 August 2022 18:46:29 |
Eccentricity: | 0.0028951 |
inclination: | 82.9281° |
perigee height: | 959 km |
apogee height: | 1002 km |
right ascension of ascending node: | 44.9935° |
argument of perigee: | 350.5638° |
revolutions per day: | 13.75303725 |
mean anomaly at epoch: | 20.1858° |
orbit number at epoch: | 52134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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