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 18140.88204447 -.00000045 +00000-0 +67053-4 0 9993
2 22078 066.0852 329.3607 0015197 240.4929 119.4574 12.86788816210943
| Epoch (UTC): | 20 May 2018 21:10:08 |
| Eccentricity: | 0.0015197 |
| inclination: | 66.0852° |
| perigee height: | 1302 km |
| apogee height: | 1326 km |
| right ascension of ascending node: | 329.3607° |
| argument of perigee: | 240.4929° |
| revolutions per day: | 12.86788816 |
| mean anomaly at epoch: | 119.4574° |
| orbit number at epoch: | 21094 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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