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 57500U 26144.78917286 +.00000000 +00000-0 +18938-3 0 00007
2 57500 43.0038 306.2981 0001032 276.5967 83.4767 15.27557502 08
| Epoch (UTC): | 24 May 2026 18:56:24 |
| Eccentricity: | 0.0001032 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.2981° |
| argument of perigee: | 276.5967° |
| revolutions per day: | 15.27557502 |
| mean anomaly at epoch: | 83.4767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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