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 39751U 14027A 20169.22222530 0.00000000 00000-0 00000-0 0 08
2 39751 2.7245 155.9004 0003771 352.9836 7.0117 1.00270000 01
| Epoch (UTC): | 17 June 2020 05:20:00 |
| Eccentricity: | 0.0003771 |
| inclination: | 2.7245° |
| perigee height: | 35771 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 155.9004° |
| argument of perigee: | 352.9836° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 7.0117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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