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 32791U 08021J 25347.23157210 .00029156 00000-0 11581-2 0 9996
2 32791 97.7445 332.3938 0001381 203.4259 156.6916 15.25283576958874
| Epoch (UTC): | 13 December 2025 05:33:27 |
| Eccentricity: | 0.0001381 |
| inclination: | 97.7445° |
| perigee height: | 489 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 332.3938° |
| argument of perigee: | 203.4259° |
| revolutions per day: | 15.25283576 |
| mean anomaly at epoch: | 156.6916° |
| orbit number at epoch: | 95887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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