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 56920U 26145.61187970 +.00000000 +00000-0 +11528-4 0 00003
2 56920 43.0032 356.1516 0000946 244.8692 115.2062 15.27574848 05
| Epoch (UTC): | 25 May 2026 14:41:06 |
| Eccentricity: | 0.0000946 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.1516° |
| argument of perigee: | 244.8692° |
| revolutions per day: | 15.27574848 |
| mean anomaly at epoch: | 115.2062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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