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 57783U 26145.40620897 +.00000000 +00000-0 +13069-3 0 00009
2 57783 43.0022 124.2984 0001482 291.3167 68.7526 15.27583229 05
| Epoch (UTC): | 25 May 2026 09:44:56 |
| Eccentricity: | 0.0001482 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.2984° |
| argument of perigee: | 291.3167° |
| revolutions per day: | 15.27583229 |
| mean anomaly at epoch: | 68.7526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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