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 43595U 98067PG 20344.55055662 .07916525 12514-4 56251-3 0 9997
2 43595 51.6588 97.6693 0009437 42.2825 52.9592 16.39998780132780
| Epoch (UTC): | 09 December 2020 13:12:48 |
| Eccentricity: | 0.0009437 |
| inclination: | 51.6588° |
| perigee height: | 159 km |
| apogee height: | 172 km |
| right ascension of ascending node: | 97.6693° |
| argument of perigee: | 42.2825° |
| revolutions per day: | 16.39998780 |
| mean anomaly at epoch: | 52.9592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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