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 43552U 98067PA 20361.21801847 .10316869 12478-4 50011-3 0 9992
2 43552 51.6122 8.3673 0000676 209.2273 150.8717 16.43170683140619
| Epoch (UTC): | 26 December 2020 05:13:56 |
| Eccentricity: | 0.0000676 |
| inclination: | 51.6122° |
| perigee height: | 157 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 8.3673° |
| argument of perigee: | 209.2273° |
| revolutions per day: | 16.43170683 |
| mean anomaly at epoch: | 150.8717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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