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 data is extracted from the following two-line orbital elements,
1 25544U 98067A 25201.26732422 .00007301 00000-0 13592-3 0 9992
2 25544 51.6337 143.1027 0002198 97.0892 263.0347 15.49967702520293
| Epoch (UTC): | 20 July 2025 06:24:56 |
| Eccentricity: | 0.0002198 |
| inclination: | 51.6337° |
| perigee height: | 415 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 143.1027° |
| argument of perigee: | 97.0892° |
| revolutions per day: | 15.49967702 |
| mean anomaly at epoch: | 263.0347° |
| orbit number at epoch: | 52029 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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