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 50161U 26145.34524963 +.00000000 +00000-0 +10523-4 0 00005
2 50161 53.2135 275.0008 0001254 82.4687 277.6447 15.08838294 08
| Epoch (UTC): | 25 May 2026 08:17:09 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 275.0008° |
| argument of perigee: | 82.4687° |
| revolutions per day: | 15.08838294 |
| mean anomaly at epoch: | 277.6447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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