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 is defined by the following mean orbital elements,
1 42718U 98067LZ 18356.15972234 .08813836 12573-4 44196-3 0 9994
2 42718 51.6191 91.1207 0006689 20.3338 341.4464 16.42542197 90809
| Epoch (UTC): | 22 December 2018 03:50:00 |
| Eccentricity: | 0.0006689 |
| inclination: | 51.6191° |
| perigee height: | 154 km |
| apogee height: | 163 km |
| right ascension of ascending node: | 91.1207° |
| argument of perigee: | 20.3338° |
| revolutions per day: | 16.42542197 |
| mean anomaly at epoch: | 341.4464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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