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 20480U 90013C 18109.84563252 -.00000037 +00000-0 -15600-4 0 9999
2 20480 099.0626 190.9733 0540821 056.8560 308.3240 12.83418459321012
Epoch (UTC): | 19 April 2018 20:17:42 |
Eccentricity: | 0.0540821 |
inclination: | 99.0626° |
perigee height: | 911 km |
apogee height: | 1744 km |
right ascension of ascending node: | 190.9733° |
argument of perigee: | 56.8560° |
revolutions per day: | 12.83418459 |
mean anomaly at epoch: | 308.3240° |
orbit number at epoch: | 32101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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