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 66518U 26145.47712668 +.00000000 +00000-0 +43804-3 0 00000
2 66518 43.0040 204.5825 0001440 276.6743 83.3945 15.27589744 03
| Epoch (UTC): | 25 May 2026 11:27:03 |
| Eccentricity: | 0.0001440 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.5825° |
| argument of perigee: | 276.6743° |
| revolutions per day: | 15.27589744 |
| mean anomaly at epoch: | 83.3945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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