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 13066U 82012B 22221.35200866 -.00000029 00000-0 -44780-4 0 9998
2 13066 82.8940 254.1030 0043980 20.6915 350.7088 13.77201749 33616
Epoch (UTC): | 09 August 2022 08:26:53 |
Eccentricity: | 0.0043980 |
inclination: | 82.8940° |
perigee height: | 941 km |
apogee height: | 1006 km |
right ascension of ascending node: | 254.1030° |
argument of perigee: | 20.6915° |
revolutions per day: | 13.77201749 |
mean anomaly at epoch: | 350.7088° |
orbit number at epoch: | 3361 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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