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 43554U 98067PC 20270.57593485 .04847927 12138-4 97747-3 0 9995
2 43554 51.6160 101.1275 0010186 278.2959 81.6908 16.30403101126085
| Epoch (UTC): | 26 September 2020 13:49:20 |
| Eccentricity: | 0.0010186 |
| inclination: | 51.6160° |
| perigee height: | 185 km |
| apogee height: | 198 km |
| right ascension of ascending node: | 101.1275° |
| argument of perigee: | 278.2959° |
| revolutions per day: | 16.30403101 |
| mean anomaly at epoch: | 81.6908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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