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 43134U 18004Z 23324.31191463 .14866072 24853-5 28500-3 0 9999
2 43134 97.2799 52.0533 0009686 279.7455 80.2754 16.46797629326864
| Epoch (UTC): | 20 November 2023 07:29:09 |
| Eccentricity: | 0.0009686 |
| inclination: | 97.2799° |
| perigee height: | 141 km |
| apogee height: | 154 km |
| right ascension of ascending node: | 52.0533° |
| argument of perigee: | 279.7455° |
| revolutions per day: | 16.46797629 |
| mean anomaly at epoch: | 80.2754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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