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 24278.83985988 .00073544 00000-0 13195-2 0 9995
2 25544 51.6398 132.2643 0008529 46.0021 40.6081 15.49204776475552
| Epoch (UTC): | 04 October 2024 20:09:23 |
| Eccentricity: | 0.0008529 |
| inclination: | 51.6398° |
| perigee height: | 413 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 132.2643° |
| argument of perigee: | 46.0021° |
| revolutions per day: | 15.49204776 |
| mean anomaly at epoch: | 40.6081° |
| orbit number at epoch: | 47555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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