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 42702U 98067LK 18066.37622415 .22640365 12480-4 12628-2 0 9994
2 42702 51.6147 131.6862 0001623 340.6009 19.7898 16.42105255 46241
| Epoch (UTC): | 07 March 2018 09:01:45 |
| Eccentricity: | 0.0001623 |
| inclination: | 51.6147° |
| perigee height: | 159 km |
| apogee height: | 161 km |
| right ascension of ascending node: | 131.6862° |
| argument of perigee: | 340.6009° |
| revolutions per day: | 16.42105255 |
| mean anomaly at epoch: | 19.7898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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