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 58865U 26145.52815369 +.00000000 +00000-0 +45240-4 0 00001
2 58865 43.0032 175.0056 0001380 273.5965 86.4729 15.27580412 00
| Epoch (UTC): | 25 May 2026 12:40:32 |
| Eccentricity: | 0.0001380 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.0056° |
| argument of perigee: | 273.5965° |
| revolutions per day: | 15.27580412 |
| mean anomaly at epoch: | 86.4729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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