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 53529U 26145.54621764 +.00000000 +00000-0 +98600-3 0 00006
2 53529 53.2144 87.0393 0002344 24.3490 335.7615 15.13600195 01
| Epoch (UTC): | 25 May 2026 13:06:33 |
| Eccentricity: | 0.0002344 |
| inclination: | 53.2144° |
| perigee height: | 524 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 87.0393° |
| argument of perigee: | 24.3490° |
| revolutions per day: | 15.13600195 |
| mean anomaly at epoch: | 335.7615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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