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 20547U 90028B 24357.88347468 .00007969 00000-0 20895-3 0 9994
2 20547 94.0851 199.7229 0067208 48.4891 312.2100 15.36386380918553
| Epoch (UTC): | 22 December 2024 21:12:12 |
| Eccentricity: | 0.0067208 |
| inclination: | 94.0851° |
| perigee height: | 411 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 199.7229° |
| argument of perigee: | 48.4891° |
| revolutions per day: | 15.36386380 |
| mean anomaly at epoch: | 312.2100° |
| orbit number at epoch: | 91855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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