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 40314U 98067FL 17070.86633509 .10752586 12608-4 10533-3 0 9997
2 40314 51.6077 46.2938 0005698 162.2115 198.1476 16.50743229182756
| Epoch (UTC): | 11 March 2017 20:47:31 |
| Eccentricity: | 0.0005698 |
| inclination: | 51.6077° |
| perigee height: | 133 km |
| apogee height: | 141 km |
| right ascension of ascending node: | 46.2938° |
| argument of perigee: | 162.2115° |
| revolutions per day: | 16.50743229 |
| mean anomaly at epoch: | 198.1476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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