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 44252U 19029T 19346.25002315 -.00026093 00000-0 -14853-2 0 9994
2 44252 53.0002 343.1889 0000932 104.7683 285.3904 15.12127856 30550
Epoch (UTC): | 12 December 2019 06:00:02 |
Eccentricity: | 0.0000932 |
inclination: | 53.0002° |
perigee height: | 529 km |
apogee height: | 530 km |
right ascension of ascending node: | 343.1889° |
argument of perigee: | 104.7683° |
revolutions per day: | 15.12127856 |
mean anomaly at epoch: | 285.3904° |
orbit number at epoch: | 3055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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