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 24286.82176872 .00028824 00000-0 51475-3 0 9992
2 25544 51.6380 92.7424 0009179 63.7262 296.4669 15.49763544476798
| Epoch (UTC): | 12 October 2024 19:43:20 |
| Eccentricity: | 0.0009179 |
| inclination: | 51.6380° |
| perigee height: | 411 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 92.7424° |
| argument of perigee: | 63.7262° |
| revolutions per day: | 15.49763544 |
| mean anomaly at epoch: | 296.4669° |
| orbit number at epoch: | 47679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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