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 42723U 98067MC 18337.56119802 .13780986 12541-4 29133-3 0 9992
2 42723 51.6259 187.6942 0006339 249.0867 110.9484 16.46458799 87542
| Epoch (UTC): | 03 December 2018 13:28:07 |
| Eccentricity: | 0.0006339 |
| inclination: | 51.6259° |
| perigee height: | 144 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 187.6942° |
| argument of perigee: | 249.0867° |
| revolutions per day: | 16.46458799 |
| mean anomaly at epoch: | 110.9484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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