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 50167U 26145.39036506 +.00000000 +00000-0 +35547-4 0 00000
2 50167 53.2148 274.8067 0001145 93.2089 266.9035 15.08836771 07
| Epoch (UTC): | 25 May 2026 09:22:07 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 274.8067° |
| argument of perigee: | 93.2089° |
| revolutions per day: | 15.08836771 |
| mean anomaly at epoch: | 266.9035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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