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 22078U 92052C 19345.80633790 -.00000064 +00000-0 -79225-5 0 9997
2 22078 066.0833 215.0072 0015846 293.0011 066.9336 12.86792639284273
Epoch (UTC): | 11 December 2019 19:21:07 |
Eccentricity: | 0.0015846 |
inclination: | 66.0833° |
perigee height: | 1302 km |
apogee height: | 1326 km |
right ascension of ascending node: | 215.0072° |
argument of perigee: | 293.0011° |
revolutions per day: | 12.86792639 |
mean anomaly at epoch: | 66.9336° |
orbit number at epoch: | 28427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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