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 66982U 26145.46644334 +.00000000 +00000-0 +10651-2 0 00001
2 66982 42.9999 309.4912 0001085 279.9016 80.1713 15.27582423 00
| Epoch (UTC): | 25 May 2026 11:11:40 |
| Eccentricity: | 0.0001085 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.4912° |
| argument of perigee: | 279.9016° |
| revolutions per day: | 15.27582423 |
| mean anomaly at epoch: | 80.1713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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