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 53595U 26145.05774628 +.00000000 +00000-0 +49860-4 0 00008
2 53595 53.2153 261.3011 0001299 91.8907 268.2234 15.08840616 03
| Epoch (UTC): | 25 May 2026 01:23:09 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.2153° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 261.3011° |
| argument of perigee: | 91.8907° |
| revolutions per day: | 15.08840616 |
| mean anomaly at epoch: | 268.2234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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