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 59240U 26145.19775866 +.00000000 +00000-0 +48599-4 0 00009
2 59240 43.0035 71.7485 0001138 273.0396 87.0325 15.27579326 04
| Epoch (UTC): | 25 May 2026 04:44:46 |
| Eccentricity: | 0.0001138 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 71.7485° |
| argument of perigee: | 273.0396° |
| revolutions per day: | 15.27579326 |
| mean anomaly at epoch: | 87.0325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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