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 56919U 26145.59388617 +.00000000 +00000-0 +53920-4 0 00001
2 56919 43.0027 356.0217 0001595 262.8197 97.2473 15.27577592 09
| Epoch (UTC): | 25 May 2026 14:15:11 |
| Eccentricity: | 0.0001595 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.0217° |
| argument of perigee: | 262.8197° |
| revolutions per day: | 15.27577592 |
| mean anomaly at epoch: | 97.2473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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