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 43157U 18008C 24103.03271106 .18194248 24335-5 16060-2 0 9991
2 43157 97.2162 161.4645 0013704 262.1472 97.8272 16.38947242344805
| Epoch (UTC): | 12 April 2024 00:47:06 |
| Eccentricity: | 0.0013704 |
| inclination: | 97.2162° |
| perigee height: | 159 km |
| apogee height: | 177 km |
| right ascension of ascending node: | 161.4645° |
| argument of perigee: | 262.1472° |
| revolutions per day: | 16.38947242 |
| mean anomaly at epoch: | 97.8272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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