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 63475U 26145.59608663 +.00000000 +00000-0 +48243-3 0 00003
2 63475 42.9983 185.8711 0001445 275.3388 84.7299 15.27594753 00
| Epoch (UTC): | 25 May 2026 14:18:21 |
| Eccentricity: | 0.0001445 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.8711° |
| argument of perigee: | 275.3388° |
| revolutions per day: | 15.27594753 |
| mean anomaly at epoch: | 84.7299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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