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 43548U 98067NW 20358.54873977 .07367411 12353-4 71823-3 0 9993
2 43548 51.6133 23.4318 0001982 43.8993 316.2190 16.37524600140249
| Epoch (UTC): | 23 December 2020 13:10:11 |
| Eccentricity: | 0.0001982 |
| inclination: | 51.6133° |
| perigee height: | 171 km |
| apogee height: | 174 km |
| right ascension of ascending node: | 23.4318° |
| argument of perigee: | 43.8993° |
| revolutions per day: | 16.37524600 |
| mean anomaly at epoch: | 316.2190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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