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 22U 59009A 25317.06399147 .00019878 00000-0 76445-3 0 9996
2 22 50.2698 84.3594 0086577 334.7551 24.9189 15.22896457767349
| Epoch (UTC): | 13 November 2025 01:32:08 |
| Eccentricity: | 0.0086577 |
| inclination: | 50.2698° |
| perigee height: | 437 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 84.3594° |
| argument of perigee: | 334.7551° |
| revolutions per day: | 15.22896457 |
| mean anomaly at epoch: | 24.9189° |
| orbit number at epoch: | 76734 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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