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 50182U 26145.35351051 +.00000000 +00000-0 +18193-4 0 00006
2 50182 53.2158 264.8072 0001323 90.8520 269.2624 15.08834762 09
| Epoch (UTC): | 25 May 2026 08:29:03 |
| Eccentricity: | 0.0001323 |
| inclination: | 53.2158° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 264.8072° |
| argument of perigee: | 90.8520° |
| revolutions per day: | 15.08834762 |
| mean anomaly at epoch: | 269.2624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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