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 42726U 98067MF 20116.07643009 .13690248 12613-4 18337-3 0 9995
2 42726 51.6113 128.9553 0003404 226.2479 133.8270 16.49117643167130
| Epoch (UTC): | 25 April 2020 01:50:03 |
| Eccentricity: | 0.0003404 |
| inclination: | 51.6113° |
| perigee height: | 139 km |
| apogee height: | 144 km |
| right ascension of ascending node: | 128.9553° |
| argument of perigee: | 226.2479° |
| revolutions per day: | 16.49117643 |
| mean anomaly at epoch: | 133.8270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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