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 59U 60013B 19348.75543382 +.00000086 +00000-0 -59939-5 0 9991
2 59 028.2486 092.0855 0189049 167.5654 192.9639 13.52972272921438
Epoch (UTC): | 14 December 2019 18:07:49 |
Eccentricity: | 0.0189049 |
inclination: | 28.2486° |
perigee height: | 921 km |
apogee height: | 1202 km |
right ascension of ascending node: | 92.0855° |
argument of perigee: | 167.5654° |
revolutions per day: | 13.52972272 |
mean anomaly at epoch: | 192.9639° |
orbit number at epoch: | 92143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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