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 11080U 78098A 18112.86854704 -.00000020 00000-0 23111-4 0 9992
2 11080 99.5196 253.0717 0008504 210.0073 150.0594 13.84294616994983
| Epoch (UTC): | 22 April 2018 20:50:42 |
| Eccentricity: | 0.0008504 |
| inclination: | 99.5196° |
| perigee height: | 942 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 253.0717° |
| argument of perigee: | 210.0073° |
| revolutions per day: | 13.84294616 |
| mean anomaly at epoch: | 150.0594° |
| orbit number at epoch: | 99498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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