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 00011U 59001A 25339.32788492 .00000586 00000-0 31139-3 0 9991
2 00011 32.8655 98.6605 1447578 33.9034 334.6137 11.90140724512368
| Epoch (UTC): | 05 December 2025 07:52:09 |
| Eccentricity: | 0.1447578 |
| inclination: | 32.8655° |
| perigee height: | 552 km |
| apogee height: | 2898 km |
| right ascension of ascending node: | 98.6605° |
| argument of perigee: | 33.9034° |
| revolutions per day: | 11.90140724 |
| mean anomaly at epoch: | 334.6137° |
| orbit number at epoch: | 51236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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