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 57522U 26145.42824867 +.00000000 +00000-0 +45914-4 0 00000
2 57522 43.0024 288.5407 0001368 270.6767 89.3928 15.27580302 05
| Epoch (UTC): | 25 May 2026 10:16:40 |
| Eccentricity: | 0.0001368 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 288.5407° |
| argument of perigee: | 270.6767° |
| revolutions per day: | 15.27580302 |
| mean anomaly at epoch: | 89.3928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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