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 53746U 26145.66679325 +.00000000 +00000-0 +46855-4 0 00002
2 53746 53.2151 278.6005 0001437 69.8604 290.2542 15.08839399 09
| Epoch (UTC): | 25 May 2026 16:00:10 |
| Eccentricity: | 0.0001437 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 278.6005° |
| argument of perigee: | 69.8604° |
| revolutions per day: | 15.08839399 |
| mean anomaly at epoch: | 290.2542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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