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 53976U 26145.41103088 +.00000000 +00000-0 +16174-3 0 00008
2 53976 53.2167 219.8228 0001722 79.8595 280.2591 15.08855365 06
| Epoch (UTC): | 25 May 2026 09:51:53 |
| Eccentricity: | 0.0001722 |
| inclination: | 53.2167° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 219.8228° |
| argument of perigee: | 79.8595° |
| revolutions per day: | 15.08855365 |
| mean anomaly at epoch: | 280.2591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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