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 data is extracted from the following two-line orbital elements,
1 22519U 92086C 24185.89103844 0.00005400 00000-0 89337-3 0 06
2 22519 56.8894 129.2737 3036806 111.7727 248.2273 9.11058018 05
| Epoch (UTC): | 03 July 2024 21:23:05 |
| Eccentricity: | 0.3036806 |
| inclination: | 56.8894° |
| perigee height: | 365 km |
| apogee height: | 6246 km |
| right ascension of ascending node: | 129.2737° |
| argument of perigee: | 111.7727° |
| revolutions per day: | 9.11058018 |
| mean anomaly at epoch: | 248.2273° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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