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 43678U 18084H 25342.58131907 .00004400 00000-0 36440-3 0 9997
2 43678 98.1024 165.8773 0007567 56.5500 303.6444 14.99402787387640
| Epoch (UTC): | 08 December 2025 13:57:05 |
| Eccentricity: | 0.0007567 |
| inclination: | 98.1024° |
| perigee height: | 563 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 165.8773° |
| argument of perigee: | 56.5500° |
| revolutions per day: | 14.99402787 |
| mean anomaly at epoch: | 303.6444° |
| orbit number at epoch: | 38764 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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