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 50814U 26145.41240904 +.00000000 +00000-0 -13481-3 0 00004
2 50814 53.2108 184.6997 0001144 96.2193 263.8930 15.08848565 04
| Epoch (UTC): | 25 May 2026 09:53:52 |
| Eccentricity: | 0.0001144 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.6997° |
| argument of perigee: | 96.2193° |
| revolutions per day: | 15.08848565 |
| mean anomaly at epoch: | 263.8930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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