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 52110U 26145.26981678 +.00000000 +00000-0 +10750-3 0 00003
2 52110 53.2134 95.3374 0001330 77.6493 282.4648 15.08841040 08
| Epoch (UTC): | 25 May 2026 06:28:32 |
| Eccentricity: | 0.0001330 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.3374° |
| argument of perigee: | 77.6493° |
| revolutions per day: | 15.08841040 |
| mean anomaly at epoch: | 282.4648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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