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 66525U 26145.45142899 +.00000000 +00000-0 +39893-3 0 00002
2 66525 42.9992 204.3851 0001564 284.7609 75.3069 15.27588499 04
| Epoch (UTC): | 25 May 2026 10:50:03 |
| Eccentricity: | 0.0001564 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3851° |
| argument of perigee: | 284.7609° |
| revolutions per day: | 15.27588499 |
| mean anomaly at epoch: | 75.3069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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