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 25166.84504551 .00008996 00000-0 16413-3 0 9992
2 25544 51.6369 313.7285 0001524 252.0477 108.0346 15.50221580514955
| Epoch (UTC): | 15 June 2025 20:16:51 |
| Eccentricity: | 0.0001524 |
| inclination: | 51.6369° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 313.7285° |
| argument of perigee: | 252.0477° |
| revolutions per day: | 15.50221580 |
| mean anomaly at epoch: | 108.0346° |
| orbit number at epoch: | 51495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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