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 66590U 26145.59967764 +.00000000 +00000-0 +50403-3 0 00005
2 66590 42.9994 342.2315 0000822 230.7860 129.2919 15.27599772 00
| Epoch (UTC): | 25 May 2026 14:23:32 |
| Eccentricity: | 0.0000822 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.2315° |
| argument of perigee: | 230.7860° |
| revolutions per day: | 15.27599772 |
| mean anomaly at epoch: | 129.2919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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