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 25190.80012176 .00007015 00000-0 30567-3 0 9996
2 22 50.2737 341.0168 0091209 193.7538 166.0932 15.19585628503083
| Epoch (UTC): | 09 July 2025 19:12:10 |
| Eccentricity: | 0.0091209 |
| inclination: | 50.2737° |
| perigee height: | 444 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 341.0168° |
| argument of perigee: | 193.7538° |
| revolutions per day: | 15.19585628 |
| mean anomaly at epoch: | 166.0932° |
| orbit number at epoch: | 50308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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