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 59689U 26145.57348436 +.00000000 +00000-0 +90938-4 0 00001
2 59689 43.0036 345.4352 0001130 270.0115 90.0607 15.27576213 03
| Epoch (UTC): | 25 May 2026 13:45:49 |
| Eccentricity: | 0.0001130 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.4352° |
| argument of perigee: | 270.0115° |
| revolutions per day: | 15.27576213 |
| mean anomaly at epoch: | 90.0607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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