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 55475U 26145.34637978 +.00000000 +00000-0 +98442-6 0 00007
2 55475 43.0030 255.9728 0001602 275.8353 84.2316 15.27574409 06
| Epoch (UTC): | 25 May 2026 08:18:47 |
| Eccentricity: | 0.0001602 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 255.9728° |
| argument of perigee: | 275.8353° |
| revolutions per day: | 15.27574409 |
| mean anomaly at epoch: | 84.2316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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