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 50837U 26145.37192847 +.00000000 +00000-0 +12673-4 0 00008
2 50837 53.2131 184.8777 0001060 65.9449 294.1654 15.08837716 03
| Epoch (UTC): | 25 May 2026 08:55:34 |
| Eccentricity: | 0.0001060 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 184.8777° |
| argument of perigee: | 65.9449° |
| revolutions per day: | 15.08837716 |
| mean anomaly at epoch: | 294.1654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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