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 is defined by the following mean orbital elements,
1 59643U 26145.48023963 +.00000000 +00000-0 +79927-3 0 00000
2 59643 43.0005 66.3274 0001311 279.8626 80.2078 15.27566374 06
| Epoch (UTC): | 25 May 2026 11:31:32 |
| Eccentricity: | 0.0001311 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.3274° |
| argument of perigee: | 279.8626° |
| revolutions per day: | 15.27566374 |
| mean anomaly at epoch: | 80.2078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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