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 20564U 90031E 24357.76876176 .00004236 00000-0 47489-3 0 9999
2 20564 89.8445 274.5778 0057697 61.0049 299.6944 14.85451746291618
| Epoch (UTC): | 22 December 2024 18:27:01 |
| Eccentricity: | 0.0057697 |
| inclination: | 89.8445° |
| perigee height: | 572 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 274.5778° |
| argument of perigee: | 61.0049° |
| revolutions per day: | 14.85451746 |
| mean anomaly at epoch: | 299.6944° |
| orbit number at epoch: | 29161 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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