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 47126U 26145.17115073 +.00000000 +00000-0 +15303-2 0 00000
2 47126 53.0769 310.5664 0001832 138.8022 221.3111 15.19585314 08
| Epoch (UTC): | 25 May 2026 04:06:27 |
| Eccentricity: | 0.0001832 |
| inclination: | 53.0769° |
| perigee height: | 506 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 310.5664° |
| argument of perigee: | 138.8022° |
| revolutions per day: | 15.19585314 |
| mean anomaly at epoch: | 221.3111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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