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 18231.11565064 -.00000060 00000-0 71689-5 0 9993
2 22078 66.0856 140.2643 0011631 216.1979 143.8253 12.86789646222749
| Epoch (UTC): | 19 August 2018 02:46:32 |
| Eccentricity: | 0.0011631 |
| inclination: | 66.0856° |
| perigee height: | 1305 km |
| apogee height: | 1323 km |
| right ascension of ascending node: | 140.2643° |
| argument of perigee: | 216.1979° |
| revolutions per day: | 12.86789646 |
| mean anomaly at epoch: | 143.8253° |
| orbit number at epoch: | 22274 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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