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 32062U 26104.09337294 +.00000000 +00000-0 +55156-4 0 00002
2 32062 98.3877 49.8804 0031233 165.5256 205.2754 14.41441354 08
| Epoch (UTC): | 14 April 2026 02:14:27 |
| Eccentricity: | 0.0031233 |
| inclination: | 98.3877° |
| perigee height: | 731 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 49.8804° |
| argument of perigee: | 165.5256° |
| revolutions per day: | 14.41441354 |
| mean anomaly at epoch: | 205.2754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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