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 53565U 26145.20131925 +.00000000 +00000-0 -10951-3 0 00008
2 53565 53.2145 70.7982 0001532 84.9534 275.1633 15.08849504 04
| Epoch (UTC): | 25 May 2026 04:49:53 |
| Eccentricity: | 0.0001532 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 70.7982° |
| argument of perigee: | 84.9534° |
| revolutions per day: | 15.08849504 |
| mean anomaly at epoch: | 275.1633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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