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 66570U 26145.64291050 +.00000000 +00000-0 +46535-3 0 00008
2 66570 43.0008 272.9187 0001062 267.4267 92.6463 15.27591134 08
| Epoch (UTC): | 25 May 2026 15:25:47 |
| Eccentricity: | 0.0001062 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.9187° |
| argument of perigee: | 267.4267° |
| revolutions per day: | 15.27591134 |
| mean anomaly at epoch: | 92.6463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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