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 23126U 94034C 24129.07817224 .00065959 50951-6 14532-2 0 9990
2 23126 6.7568 138.6521 6208930 95.0902 333.8012 3.81291166318130
| Epoch (UTC): | 08 May 2024 01:52:34 |
| Eccentricity: | 0.6208930 |
| inclination: | 6.7568° |
| perigee height: | 183 km |
| apogee height: | 21675 km |
| right ascension of ascending node: | 138.6521° |
| argument of perigee: | 95.0902° |
| revolutions per day: | 3.81291166 |
| mean anomaly at epoch: | 333.8012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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