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 63631U 26145.53627441 +.00000000 +00000-0 +15104-3 0 00006
2 63631 45.3913 93.4443 0001129 177.7425 182.3459 14.99527578 08
| Epoch (UTC): | 25 May 2026 12:52:14 |
| Eccentricity: | 0.0001129 |
| inclination: | 45.3913° |
| perigee height: | 568 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 93.4443° |
| argument of perigee: | 177.7425° |
| revolutions per day: | 14.99527578 |
| mean anomaly at epoch: | 182.3459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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