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 50479U 26145.61370823 +.00000000 +00000-0 -14358-2 0 00000
2 50479 87.8917 25.5584 0002294 83.8256 276.3133 13.11415714 08
| Epoch (UTC): | 25 May 2026 14:43:44 |
| Eccentricity: | 0.0002294 |
| inclination: | 87.8917° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5584° |
| argument of perigee: | 83.8256° |
| revolutions per day: | 13.11415714 |
| mean anomaly at epoch: | 276.3133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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