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 65458U 26144.74125919 +.00000000 +00000-0 +50259-3 0 00000
2 65458 53.1604 264.5052 0001166 75.4958 284.6173 15.31724364 02
| Epoch (UTC): | 24 May 2026 17:47:24 |
| Eccentricity: | 0.0001166 |
| inclination: | 53.1604° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 264.5052° |
| argument of perigee: | 75.4958° |
| revolutions per day: | 15.31724364 |
| mean anomaly at epoch: | 284.6173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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