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 47086U 91056DL 24258.16970452 .00024596 00000-0 12418-1 0 9994
2 47086 82.5537 57.4268 0012911 133.9616 226.2629 14.16028809199122
| Epoch (UTC): | 14 September 2024 04:04:22 |
| Eccentricity: | 0.0012911 |
| inclination: | 82.5537° |
| perigee height: | 829 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 57.4268° |
| argument of perigee: | 133.9616° |
| revolutions per day: | 14.16028809 |
| mean anomaly at epoch: | 226.2629° |
| orbit number at epoch: | 19912 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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