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 53951U 22057BC 24250.44134991 .10334324 26218-5 10528-2 0 9999
2 53951 97.5447 27.2555 0013577 279.3123 80.6640 16.37697121127554
| Epoch (UTC): | 06 September 2024 10:35:32 |
| Eccentricity: | 0.0013577 |
| inclination: | 97.5447° |
| perigee height: | 163 km |
| apogee height: | 181 km |
| right ascension of ascending node: | 27.2555° |
| argument of perigee: | 279.3123° |
| revolutions per day: | 16.37697121 |
| mean anomaly at epoch: | 80.6640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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