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 63559U 26145.44108444 +.00000000 +00000-0 +14849-2 0 00006
2 63559 43.0011 50.8056 0000868 279.6014 80.4755 15.70882989 00
| Epoch (UTC): | 25 May 2026 10:35:09 |
| Eccentricity: | 0.0000868 |
| inclination: | 43.0011° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 50.8056° |
| argument of perigee: | 279.6014° |
| revolutions per day: | 15.70882989 |
| mean anomaly at epoch: | 80.4755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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