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 00022U 59009A 25317.19522484 .00022199 00000-0 85152-3 0 9997
2 00022 50.2698 83.7165 0086557 335.2787 24.4036 15.22907214767363
| Epoch (UTC): | 13 November 2025 04:41:07 |
| Eccentricity: | 0.0086557 |
| inclination: | 50.2698° |
| perigee height: | 437 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 83.7165° |
| argument of perigee: | 335.2787° |
| revolutions per day: | 15.22907214 |
| mean anomaly at epoch: | 24.4036° |
| orbit number at epoch: | 76736 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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