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 27601U 02056E 21110.56165455 -.00000018 00000-0 80323-5 0 9992
2 27601 98.1949 135.9945 0073424 82.7443 29.7801 14.31990817958644
Epoch (UTC): | 20 April 2021 13:28:46 |
Eccentricity: | 0.0073424 |
inclination: | 98.1949° |
perigee height: | 732 km |
apogee height: | 837 km |
right ascension of ascending node: | 135.9945° |
argument of perigee: | 82.7443° |
revolutions per day: | 14.31990817 |
mean anomaly at epoch: | 29.7801° |
orbit number at epoch: | 95864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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