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 43467U 98067NQ 20362.27906033 .06269310 12352-4 52456-3 0 9996
2 43467 51.6190 354.3668 0001241 137.3285 222.7838 16.38845679150702
| Epoch (UTC): | 27 December 2020 06:41:50 |
| Eccentricity: | 0.0001241 |
| inclination: | 51.6190° |
| perigee height: | 168 km |
| apogee height: | 169 km |
| right ascension of ascending node: | 354.3668° |
| argument of perigee: | 137.3285° |
| revolutions per day: | 16.38845679 |
| mean anomaly at epoch: | 222.7838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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