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 66529U 26145.21815521 +.00000000 +00000-0 +55884-3 0 00007
2 66529 43.0027 206.0774 0001559 267.0874 92.9799 15.27591637 07
| Epoch (UTC): | 25 May 2026 05:14:08 |
| Eccentricity: | 0.0001559 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 206.0774° |
| argument of perigee: | 267.0874° |
| revolutions per day: | 15.27591637 |
| mean anomaly at epoch: | 92.9799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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