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 42730U 98067MK 19079.94531326 .10885211 12450-4 35996-3 0 9992
2 42730 51.6143 358.5732 0006672 231.8651 128.1776 16.44308785104146
| Epoch (UTC): | 20 March 2019 22:41:15 |
| Eccentricity: | 0.0006672 |
| inclination: | 51.6143° |
| perigee height: | 150 km |
| apogee height: | 159 km |
| right ascension of ascending node: | 358.5732° |
| argument of perigee: | 231.8651° |
| revolutions per day: | 16.44308785 |
| mean anomaly at epoch: | 128.1776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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