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 57650U 26145.62198333 +.00000000 +00000-0 -47956-5 0 00006
2 57650 43.0037 17.9497 0000886 276.0037 84.0714 15.27583707 05
| Epoch (UTC): | 25 May 2026 14:55:39 |
| Eccentricity: | 0.0000886 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 17.9497° |
| argument of perigee: | 276.0037° |
| revolutions per day: | 15.27583707 |
| mean anomaly at epoch: | 84.0714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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