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 43589U 98067PD 20325.00934518 .09147399 12394-4 58853-3 0 9998
2 43589 51.6128 191.6935 0007320 255.9940 104.0273 16.40872661130679
| Epoch (UTC): | 20 November 2020 00:13:27 |
| Eccentricity: | 0.0007320 |
| inclination: | 51.6128° |
| perigee height: | 159 km |
| apogee height: | 168 km |
| right ascension of ascending node: | 191.6935° |
| argument of perigee: | 255.9940° |
| revolutions per day: | 16.40872661 |
| mean anomaly at epoch: | 104.0273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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