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 59362U 26145.47299071 +.00000000 +00000-0 +86506-4 0 00004
2 59362 43.0010 186.4118 0001241 276.0844 83.9866 15.27567440 04
| Epoch (UTC): | 25 May 2026 11:21:06 |
| Eccentricity: | 0.0001241 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.4118° |
| argument of perigee: | 276.0844° |
| revolutions per day: | 15.27567440 |
| mean anomaly at epoch: | 83.9866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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