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 57257U 26145.47594625 +.00000000 +00000-0 +38577-4 0 00003
2 57257 43.0033 306.2205 0001230 250.5783 109.4936 15.27579326 04
| Epoch (UTC): | 25 May 2026 11:25:21 |
| Eccentricity: | 0.0001230 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.2205° |
| argument of perigee: | 250.5783° |
| revolutions per day: | 15.27579326 |
| mean anomaly at epoch: | 109.4936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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