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 51658U 22013C 24311.77390724 .18631335 26304-5 25968-3 0 9996
2 51658 97.4678 343.7865 0009075 272.1309 87.8956 16.48726192152264
| Epoch (UTC): | 06 November 2024 18:34:25 |
| Eccentricity: | 0.0009075 |
| inclination: | 97.4678° |
| perigee height: | 137 km |
| apogee height: | 148 km |
| right ascension of ascending node: | 343.7865° |
| argument of perigee: | 272.1309° |
| revolutions per day: | 16.48726192 |
| mean anomaly at epoch: | 87.8956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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