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 25340.58693591 .00000611 00000-0 32520-3 0 9990
2 00011 32.8657 93.8968 1447556 41.0670 329.0304 11.90142332512519
| Epoch (UTC): | 06 December 2025 14:05:11 |
| Eccentricity: | 0.1447556 |
| inclination: | 32.8657° |
| perigee height: | 552 km |
| apogee height: | 2898 km |
| right ascension of ascending node: | 93.8968° |
| argument of perigee: | 41.0670° |
| revolutions per day: | 11.90142332 |
| mean anomaly at epoch: | 329.0304° |
| orbit number at epoch: | 51251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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