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 40910U 15049M 19345.81431919 .00000899 00000-0 48063-4 0 9992
2 40910 97.4649 347.0012 0013351 301.1835 183.1110 15.17586680233725
Epoch (UTC): | 11 December 2019 19:32:37 |
Eccentricity: | 0.0013351 |
inclination: | 97.4649° |
perigee height: | 504 km |
apogee height: | 522 km |
right ascension of ascending node: | 347.0012° |
argument of perigee: | 301.1835° |
revolutions per day: | 15.17586680 |
mean anomaly at epoch: | 183.1110° |
orbit number at epoch: | 23372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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