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 53608U 26145.27213250 +.00000000 +00000-0 +15219-4 0 00007
2 53608 53.2149 250.5206 0001181 86.9640 273.1488 15.08835904 08
| Epoch (UTC): | 25 May 2026 06:31:52 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 250.5206° |
| argument of perigee: | 86.9640° |
| revolutions per day: | 15.08835904 |
| mean anomaly at epoch: | 273.1488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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