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 63786U 26145.53468897 +.00000000 +00000-0 +88984-3 0 00001
2 63786 43.0029 338.6353 0001879 262.4647 97.5991 15.27587135 01
| Epoch (UTC): | 25 May 2026 12:49:57 |
| Eccentricity: | 0.0001879 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.6353° |
| argument of perigee: | 262.4647° |
| revolutions per day: | 15.27587135 |
| mean anomaly at epoch: | 97.5991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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