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 20666U 90055D 22222.07320894 .00001032 00000-0 10014-3 0 9997
2 20666 62.7852 344.7541 0131407 77.7459 283.8314 14.93360769741734
Epoch (UTC): | 10 August 2022 01:45:25 |
Eccentricity: | 0.0131407 |
inclination: | 62.7852° |
perigee height: | 496 km |
apogee height: | 679 km |
right ascension of ascending node: | 344.7541° |
argument of perigee: | 77.7459° |
revolutions per day: | 14.93360769 |
mean anomaly at epoch: | 283.8314° |
orbit number at epoch: | 74173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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