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 53544U 26145.52694831 +.00000000 +00000-0 +50345-4 0 00001
2 53544 53.2125 79.1837 0001218 94.4645 265.6486 15.08840648 01
| Epoch (UTC): | 25 May 2026 12:38:48 |
| Eccentricity: | 0.0001218 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 79.1837° |
| argument of perigee: | 94.4645° |
| revolutions per day: | 15.08840648 |
| mean anomaly at epoch: | 265.6486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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