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 25344.61643645 .00017287 00000-0 65257-3 0 9993
2 22 50.2573 309.3249 0085845 85.6846 275.3916 15.23665104771545
| Epoch (UTC): | 10 December 2025 14:47:40 |
| Eccentricity: | 0.0085845 |
| inclination: | 50.2573° |
| perigee height: | 436 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 309.3249° |
| argument of perigee: | 85.6846° |
| revolutions per day: | 15.23665104 |
| mean anomaly at epoch: | 275.3916° |
| orbit number at epoch: | 77154 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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