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 59569U 26145.46370272 +.00000000 +00000-0 +23142-4 0 00002
2 59569 43.0034 292.0206 0001694 270.4594 89.6063 15.27577579 09
| Epoch (UTC): | 25 May 2026 11:07:43 |
| Eccentricity: | 0.0001694 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 292.0206° |
| argument of perigee: | 270.4594° |
| revolutions per day: | 15.27577579 |
| mean anomaly at epoch: | 89.6063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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