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 63014U 26145.13772832 +.00000000 +00000-0 +13802-2 0 00004
2 63014 43.0031 94.8433 0001584 235.9644 124.1073 15.70869654 08
| Epoch (UTC): | 25 May 2026 03:18:19 |
| Eccentricity: | 0.0001584 |
| inclination: | 43.0031° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 94.8433° |
| argument of perigee: | 235.9644° |
| revolutions per day: | 15.70869654 |
| mean anomaly at epoch: | 124.1073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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