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 27386U 02009A 19339.82226358 .00000016 00000-0 18669-4 0 9999
2 27386 98.1417 352.0758 0001335 91.5166 81.3916 14.37964902930643
Epoch (UTC): | 05 December 2019 19:44:03 |
Eccentricity: | 0.0001335 |
inclination: | 98.1417° |
perigee height: | 764 km |
apogee height: | 766 km |
right ascension of ascending node: | 352.0758° |
argument of perigee: | 91.5166° |
revolutions per day: | 14.37964902 |
mean anomaly at epoch: | 81.3916° |
orbit number at epoch: | 93064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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