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 25735U 99026A 23292.90378023 .11815262 24869-5 99458-4 0 9997
2 25735 97.1796 153.7521 0008248 263.9739 96.0628 16.52065812365874
| Epoch (UTC): | 19 October 2023 21:41:26 |
| Eccentricity: | 0.0008248 |
| inclination: | 97.1796° |
| perigee height: | 128 km |
| apogee height: | 139 km |
| right ascension of ascending node: | 153.7521° |
| argument of perigee: | 263.9739° |
| revolutions per day: | 16.52065812 |
| mean anomaly at epoch: | 96.0628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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