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 63566U 26145.47150565 +.00000000 +00000-0 +22412-3 0 00004
2 63566 43.0024 196.6515 0001962 276.2590 83.8038 15.27579501 05
| Epoch (UTC): | 25 May 2026 11:18:58 |
| Eccentricity: | 0.0001962 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.6515° |
| argument of perigee: | 276.2590° |
| revolutions per day: | 15.27579501 |
| mean anomaly at epoch: | 83.8038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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