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 66512U 26145.42315598 +.00000000 +00000-0 +74450-3 0 00001
2 66512 43.0024 277.3957 0001515 269.0222 91.0456 15.27590103 08
| Epoch (UTC): | 25 May 2026 10:09:20 |
| Eccentricity: | 0.0001515 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.3957° |
| argument of perigee: | 269.0222° |
| revolutions per day: | 15.27590103 |
| mean anomaly at epoch: | 91.0456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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