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 57252U 26145.51434759 +.00000000 +00000-0 +69690-4 0 00004
2 57252 43.0037 305.6492 0002054 274.3495 85.7122 15.27583117 09
| Epoch (UTC): | 25 May 2026 12:20:39 |
| Eccentricity: | 0.0002054 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 305.6492° |
| argument of perigee: | 274.3495° |
| revolutions per day: | 15.27583117 |
| mean anomaly at epoch: | 85.7122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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