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 24287.46659629 .00028395 00000-0 50666-3 0 9993
2 25544 51.6381 89.5489 0009128 65.4963 294.6976 15.49796863476897
| Epoch (UTC): | 13 October 2024 11:11:53 |
| Eccentricity: | 0.0009128 |
| inclination: | 51.6381° |
| perigee height: | 411 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 89.5489° |
| argument of perigee: | 65.4963° |
| revolutions per day: | 15.49796863 |
| mean anomaly at epoch: | 294.6976° |
| orbit number at epoch: | 47689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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