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 06779U 71116B 21100.45102972 .00000051 00000-0 99679-3 0 9998
2 06779 27.7460 269.9298 7202963 235.3707 64.1131 2.19607477373875
Epoch (UTC): | 10 April 2021 10:49:28 |
Eccentricity: | 0.7202963 |
inclination: | 27.7460° |
perigee height: | 615 km |
apogee height: | 36632 km |
right ascension of ascending node: | 269.9298° |
argument of perigee: | 235.3707° |
revolutions per day: | 2.19607477 |
mean anomaly at epoch: | 64.1131° |
orbit number at epoch: | 37387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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