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 58640U 26145.54011316 +.00000000 +00000-0 -65559-4 0 00000
2 58640 43.0058 345.3896 0001421 273.1845 86.8844 15.27579869 08
| Epoch (UTC): | 25 May 2026 12:57:45 |
| Eccentricity: | 0.0001421 |
| inclination: | 43.0058° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.3896° |
| argument of perigee: | 273.1845° |
| revolutions per day: | 15.27579869 |
| mean anomaly at epoch: | 86.8844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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