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 57153U 26145.53790792 +.00000000 +00000-0 +58378-4 0 00009
2 57153 43.0027 178.2622 0002060 311.1730 48.8943 15.27575622 09
| Epoch (UTC): | 25 May 2026 12:54:35 |
| Eccentricity: | 0.0002060 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 178.2622° |
| argument of perigee: | 311.1730° |
| revolutions per day: | 15.27575622 |
| mean anomaly at epoch: | 48.8943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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