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 42910U 98067MZ 19293.66077481 .08093820 12441-4 64211-3 0 9992
2 42910 51.6167 353.5295 0003841 355.3485 137.8062 16.39261620124803
Epoch (UTC): | 20 October 2019 15:51:30 |
Eccentricity: | 0.0003841 |
inclination: | 51.6167° |
perigee height: | 165 km |
apogee height: | 170 km |
right ascension of ascending node: | 353.5295° |
argument of perigee: | 355.3485° |
revolutions per day: | 16.39261620 |
mean anomaly at epoch: | 137.8062° |
orbit number at epoch: | 12480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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