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 57966U 26145.02616601 +.00000000 +00000-0 +23105-4 0 00001
2 57966 43.0022 264.6818 0001376 264.9464 95.1231 15.27581193 06
| Epoch (UTC): | 25 May 2026 00:37:40 |
| Eccentricity: | 0.0001376 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 264.6818° |
| argument of perigee: | 264.9464° |
| revolutions per day: | 15.27581193 |
| mean anomaly at epoch: | 95.1231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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