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 18322.51502661 -.00000043 00000-0 76681-4 0 9999
2 22078 66.0850 308.7213 0006345 187.9439 172.1480 12.86790684234507
| Epoch (UTC): | 18 November 2018 12:21:38 |
| Eccentricity: | 0.0006345 |
| inclination: | 66.0850° |
| perigee height: | 1309 km |
| apogee height: | 1319 km |
| right ascension of ascending node: | 308.7213° |
| argument of perigee: | 187.9439° |
| revolutions per day: | 12.86790684 |
| mean anomaly at epoch: | 172.1480° |
| orbit number at epoch: | 23450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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