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 50851U 26145.41883510 +.00000000 +00000-0 -80020-4 0 00005
2 50851 53.2106 194.5942 0001704 68.0382 292.0791 15.08845695 02
| Epoch (UTC): | 25 May 2026 10:03:07 |
| Eccentricity: | 0.0001704 |
| inclination: | 53.2106° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.5942° |
| argument of perigee: | 68.0382° |
| revolutions per day: | 15.08845695 |
| mean anomaly at epoch: | 292.0791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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