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 51753U 26145.47776972 +.00000000 +00000-0 +28561-4 0 00007
2 51753 53.2133 324.4149 0001384 88.1737 271.9414 15.08834353 05
| Epoch (UTC): | 25 May 2026 11:27:59 |
| Eccentricity: | 0.0001384 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 324.4149° |
| argument of perigee: | 88.1737° |
| revolutions per day: | 15.08834353 |
| mean anomaly at epoch: | 271.9414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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