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 57135U 26145.43910350 +.00000000 +00000-0 -75004-4 0 00008
2 57135 43.0002 189.7020 0001249 287.5478 72.5237 15.27575284 08
| Epoch (UTC): | 25 May 2026 10:32:18 |
| Eccentricity: | 0.0001249 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.7020° |
| argument of perigee: | 287.5478° |
| revolutions per day: | 15.27575284 |
| mean anomaly at epoch: | 72.5237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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