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 37638U 78026HZ 24355.46042832 .00001738 00000-0 94737-3 0 9990
2 37638 98.8778 250.9748 0055957 188.5869 171.4350 14.12665220521847
| Epoch (UTC): | 20 December 2024 11:03:01 |
| Eccentricity: | 0.0055957 |
| inclination: | 98.8778° |
| perigee height: | 810 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 250.9748° |
| argument of perigee: | 188.5869° |
| revolutions per day: | 14.12665220 |
| mean anomaly at epoch: | 171.4350° |
| orbit number at epoch: | 52184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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