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 50475U 26145.43061213 +.00000000 +00000-0 +13234-2 0 00007
2 50475 87.8904 25.5961 0001794 89.5806 270.5528 13.11415139 02
| Epoch (UTC): | 25 May 2026 10:20:04 |
| Eccentricity: | 0.0001794 |
| inclination: | 87.8904° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5961° |
| argument of perigee: | 89.5806° |
| revolutions per day: | 13.11415139 |
| mean anomaly at epoch: | 270.5528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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