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 59086U 26145.55895811 +.00000000 +00000-0 +26626-4 0 00007
2 59086 43.0004 236.9301 0001040 272.6218 87.4514 15.27584894 00
| Epoch (UTC): | 25 May 2026 13:24:53 |
| Eccentricity: | 0.0001040 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.9301° |
| argument of perigee: | 272.6218° |
| revolutions per day: | 15.27584894 |
| mean anomaly at epoch: | 87.4514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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