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 53184U 26145.24537580 +.00000000 +00000-0 +49879-4 0 00007
2 53184 53.2139 140.0332 0001263 76.0040 284.1093 15.08841524 03
| Epoch (UTC): | 25 May 2026 05:53:20 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 140.0332° |
| argument of perigee: | 76.0040° |
| revolutions per day: | 15.08841524 |
| mean anomaly at epoch: | 284.1093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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