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 11574U 79089B 25131.79806446 .00000367 00000-0 11944-3 0 9995
2 11574 74.0681 289.7406 0015748 182.1108 177.9985 14.42120266392589
| Epoch (UTC): | 11 May 2025 19:09:12 |
| Eccentricity: | 0.0015748 |
| inclination: | 74.0681° |
| perigee height: | 740 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 289.7406° |
| argument of perigee: | 182.1108° |
| revolutions per day: | 14.42120266 |
| mean anomaly at epoch: | 177.9985° |
| orbit number at epoch: | 39258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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