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 56879U 26144.91268705 +.00000000 +00000-0 -54475-6 0 00005
2 56879 43.0056 15.0752 0001482 269.0024 91.0657 15.27571242 07
| Epoch (UTC): | 24 May 2026 21:54:16 |
| Eccentricity: | 0.0001482 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 15.0752° |
| argument of perigee: | 269.0024° |
| revolutions per day: | 15.27571242 |
| mean anomaly at epoch: | 91.0657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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