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 24278.51847516 -.02634131 00000-0 -54276-1 0 9997
2 25544 51.6341 133.8402 0007303 74.5956 18.5068 15.48940184475505
| Epoch (UTC): | 04 October 2024 12:26:36 |
| Eccentricity: | 0.0007303 |
| inclination: | 51.6341° |
| perigee height: | 415 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 133.8402° |
| argument of perigee: | 74.5956° |
| revolutions per day: | 15.48940184 |
| mean anomaly at epoch: | 18.5068° |
| orbit number at epoch: | 47550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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