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 57976U 26145.36079978 +.00000000 +00000-0 +17904-3 0 00008
2 57976 43.0032 262.8238 0001280 276.3169 83.7537 15.27582791 04
| Epoch (UTC): | 25 May 2026 08:39:33 |
| Eccentricity: | 0.0001280 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 262.8238° |
| argument of perigee: | 276.3169° |
| revolutions per day: | 15.27582791 |
| mean anomaly at epoch: | 83.7537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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