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 57772U 26145.41006822 +.00000000 +00000-0 +32134-4 0 00009
2 57772 43.0037 124.3215 0001673 282.5281 77.5383 15.27580564 06
| Epoch (UTC): | 25 May 2026 09:50:29 |
| Eccentricity: | 0.0001673 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.3215° |
| argument of perigee: | 282.5281° |
| revolutions per day: | 15.27580564 |
| mean anomaly at epoch: | 77.5383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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