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 25349.65093408 .00000296 00000-0 15924-3 0 9996
2 00011 32.8674 59.6070 1447574 92.6299 284.0238 11.90151408513590
| Epoch (UTC): | 15 December 2025 15:37:20 |
| Eccentricity: | 0.1447574 |
| inclination: | 32.8674° |
| perigee height: | 552 km |
| apogee height: | 2898 km |
| right ascension of ascending node: | 59.6070° |
| argument of perigee: | 92.6299° |
| revolutions per day: | 11.90151408 |
| mean anomaly at epoch: | 284.0238° |
| orbit number at epoch: | 51359 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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