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 57951U 26145.40807648 +.00000000 +00000-0 -26584-4 0 00005
2 57951 53.1621 27.5313 0001529 94.1533 265.9645 15.34375806 09
| Epoch (UTC): | 25 May 2026 09:47:37 |
| Eccentricity: | 0.0001529 |
| inclination: | 53.1621° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 27.5313° |
| argument of perigee: | 94.1533° |
| revolutions per day: | 15.34375806 |
| mean anomaly at epoch: | 265.9645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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