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 25343.82942719 .00016860 00000-0 63735-3 0 9994
2 22 50.2578 313.1846 0085848 82.4992 278.5710 15.23638447771420
| Epoch (UTC): | 09 December 2025 19:54:22 |
| Eccentricity: | 0.0085848 |
| inclination: | 50.2578° |
| perigee height: | 436 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 313.1846° |
| argument of perigee: | 82.4992° |
| revolutions per day: | 15.23638447 |
| mean anomaly at epoch: | 278.5710° |
| orbit number at epoch: | 77142 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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