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 43116U 18004F 23318.00563449 .05200883 24246-5 12658-2 0 9999
2 43116 97.3099 46.1842 0009559 280.0106 80.0109 16.29277617325842
| Epoch (UTC): | 14 November 2023 00:08:06 |
| Eccentricity: | 0.0009559 |
| inclination: | 97.3099° |
| perigee height: | 188 km |
| apogee height: | 201 km |
| right ascension of ascending node: | 46.1842° |
| argument of perigee: | 280.0106° |
| revolutions per day: | 16.29277617 |
| mean anomaly at epoch: | 80.0109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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