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 43027U 98067NL 19066.21822070 .27976699 12582-4 67924-3 0 9998
2 43027 51.6122 93.2605 0000010 179.6888 180.8884 16.46418237 73939
| Epoch (UTC): | 07 March 2019 05:14:14 |
| Eccentricity: | 0.0000010 |
| inclination: | 51.6122° |
| perigee height: | 149 km |
| apogee height: | 149 km |
| right ascension of ascending node: | 93.2605° |
| argument of perigee: | 179.6888° |
| revolutions per day: | 16.46418237 |
| mean anomaly at epoch: | 180.8884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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