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 50820U 26145.52281117 +.00000000 +00000-0 +72009-4 0 00005
2 50820 53.2121 184.2042 0001586 63.4479 296.6675 15.08842056 05
| Epoch (UTC): | 25 May 2026 12:32:50 |
| Eccentricity: | 0.0001586 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.2042° |
| argument of perigee: | 63.4479° |
| revolutions per day: | 15.08842056 |
| mean anomaly at epoch: | 296.6675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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