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 50166U 26145.34711878 +.00000000 +00000-0 -36897-4 0 00006
2 50166 53.2144 264.9249 0001315 81.9748 278.1393 15.08840070 08
| Epoch (UTC): | 25 May 2026 08:19:51 |
| Eccentricity: | 0.0001315 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 264.9249° |
| argument of perigee: | 81.9748° |
| revolutions per day: | 15.08840070 |
| mean anomaly at epoch: | 278.1393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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