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 57232U 26145.51433419 +.00000000 +00000-0 +14998-4 0 00005
2 57232 43.0030 316.9454 0001203 272.8809 87.1905 15.27580653 07
| Epoch (UTC): | 25 May 2026 12:20:38 |
| Eccentricity: | 0.0001203 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.9454° |
| argument of perigee: | 272.8809° |
| revolutions per day: | 15.27580653 |
| mean anomaly at epoch: | 87.1905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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