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 53543U 26145.54903559 +.00000000 +00000-0 -17716-4 0 00008
2 53543 53.2134 79.1517 0001219 104.0844 256.0284 15.08840049 00
| Epoch (UTC): | 25 May 2026 13:10:36 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 79.1517° |
| argument of perigee: | 104.0844° |
| revolutions per day: | 15.08840049 |
| mean anomaly at epoch: | 256.0284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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