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 66588U 26145.54828219 +.00000000 +00000-0 +61008-3 0 00001
2 66588 43.0022 341.8505 0001027 270.8397 89.2337 15.27595283 07
| Epoch (UTC): | 25 May 2026 13:09:31 |
| Eccentricity: | 0.0001027 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.8505° |
| argument of perigee: | 270.8397° |
| revolutions per day: | 15.27595283 |
| mean anomaly at epoch: | 89.2337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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