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 25194.43411487 .00010152 00000-0 18227-3 0 9995
2 25544 51.6340 176.9702 0002675 6.8375 353.2650 15.50520436519237
| Epoch (UTC): | 13 July 2025 10:25:07 |
| Eccentricity: | 0.0002675 |
| inclination: | 51.6340° |
| perigee height: | 413 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 176.9702° |
| argument of perigee: | 6.8375° |
| revolutions per day: | 15.50520436 |
| mean anomaly at epoch: | 353.2650° |
| orbit number at epoch: | 51923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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