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 56296U 26145.23687597 +.00000000 +00000-0 +84536-5 0 00007
2 56296 43.0037 96.8356 0001414 272.1781 87.8909 15.27570441 09
| Epoch (UTC): | 25 May 2026 05:41:06 |
| Eccentricity: | 0.0001414 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.8356° |
| argument of perigee: | 272.1781° |
| revolutions per day: | 15.27570441 |
| mean anomaly at epoch: | 87.8909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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