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 25544U 26131.16675675 +.00000000 +00000-0 +10622-3 0 00003
2 25544 51.6310 123.3566 0007470 46.3627 313.7980 15.49181925 06
| Epoch (UTC): | 11 May 2026 04:00:07 |
| Eccentricity: | 0.0007470 |
| inclination: | 51.6310° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 123.3566° |
| argument of perigee: | 46.3627° |
| revolutions per day: | 15.49181925 |
| mean anomaly at epoch: | 313.7980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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