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 50185U 26145.58169606 +.00000000 +00000-0 +53730-4 0 00003
2 50185 53.2155 263.9746 0001213 87.4197 272.6934 15.08835214 02
| Epoch (UTC): | 25 May 2026 13:57:38 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 263.9746° |
| argument of perigee: | 87.4197° |
| revolutions per day: | 15.08835214 |
| mean anomaly at epoch: | 272.6934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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