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 62566U 26145.41163741 +.00000000 +00000-0 +19476-3 0 00003
2 62566 43.0027 37.8970 0001989 270.0648 89.9991 15.70841182 03
| Epoch (UTC): | 25 May 2026 09:52:45 |
| Eccentricity: | 0.0001989 |
| inclination: | 43.0027° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 37.8970° |
| argument of perigee: | 270.0648° |
| revolutions per day: | 15.70841182 |
| mean anomaly at epoch: | 89.9991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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