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 23757U 95074A 18120.30651581 .09692617 -16433-4 45842-3 0 9998
2 23757 22.9731 345.4866 0006325 290.6439 69.3393 16.42913300248180
| Epoch (UTC): | 30 April 2018 07:21:22 |
| Eccentricity: | 0.0006325 |
| inclination: | 22.9731° |
| perigee height: | 154 km |
| apogee height: | 162 km |
| right ascension of ascending node: | 345.4866° |
| argument of perigee: | 290.6439° |
| revolutions per day: | 16.42913300 |
| mean anomaly at epoch: | 69.3393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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