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 59695U 26145.54711859 +.00000000 +00000-0 +59437-4 0 00007
2 59695 43.0049 342.5605 0001485 262.2431 97.8252 15.27576350 03
| Epoch (UTC): | 25 May 2026 13:07:51 |
| Eccentricity: | 0.0001485 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.5605° |
| argument of perigee: | 262.2431° |
| revolutions per day: | 15.27576350 |
| mean anomaly at epoch: | 97.8252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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