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 42707U 98067LQ 19034.96093632 .08699549 12398-4 73318-3 0 9997
2 42707 51.6151 225.9993 0006204 290.2952 69.7401 16.38701088 98669
| Epoch (UTC): | 03 February 2019 23:03:44 |
| Eccentricity: | 0.0006204 |
| inclination: | 51.6151° |
| perigee height: | 165 km |
| apogee height: | 173 km |
| right ascension of ascending node: | 225.9993° |
| argument of perigee: | 290.2952° |
| revolutions per day: | 16.38701088 |
| mean anomaly at epoch: | 69.7401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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