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 55472U 26145.34089775 +.00000000 +00000-0 -19400-3 0 00005
2 55472 43.0035 248.9056 0002033 275.4616 84.6003 15.27591792 02
| Epoch (UTC): | 25 May 2026 08:10:53 |
| Eccentricity: | 0.0002033 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 248.9056° |
| argument of perigee: | 275.4616° |
| revolutions per day: | 15.27591792 |
| mean anomaly at epoch: | 84.6003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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