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 53U 60009E 24262.15002011 .00000045 00000-0 12741-2 0 9995
2 53 47.2754 147.3337 0100543 353.3584 6.5869 12.17348921857823
| Epoch (UTC): | 18 September 2024 03:36:01 |
| Eccentricity: | 0.0100543 |
| inclination: | 47.2754° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 147.3337° |
| argument of perigee: | 353.3584° |
| revolutions per day: | 12.17348921 |
| mean anomaly at epoch: | 6.5869° |
| orbit number at epoch: | 85782 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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