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 56110U 26145.54674421 +.00000000 +00000-0 +14049-4 0 00009
2 56110 43.0024 87.6857 0000941 265.7715 94.3029 15.27573920 04
| Epoch (UTC): | 25 May 2026 13:07:18 |
| Eccentricity: | 0.0000941 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.6857° |
| argument of perigee: | 265.7715° |
| revolutions per day: | 15.27573920 |
| mean anomaly at epoch: | 94.3029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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