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 11672U 80005B 21065.92674931 .00000127 00000-0 11049-4 0 9994
2 11672 82.5135 236.7364 0017990 123.2505 237.0439 14.88033787204337
Epoch (UTC): | 06 March 2021 22:14:31 |
Eccentricity: | 0.0017990 |
inclination: | 82.5135° |
perigee height: | 591 km |
apogee height: | 616 km |
right ascension of ascending node: | 236.7364° |
argument of perigee: | 123.2505° |
revolutions per day: | 14.88033787 |
mean anomaly at epoch: | 237.0439° |
orbit number at epoch: | 20433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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