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 25347.95320282 .00018733 00000-0 74560-3 0 9992
2 32791 97.7441 333.1406 0001457 198.6890 161.4294 15.25310297958985
| Epoch (UTC): | 13 December 2025 22:52:36 |
| Eccentricity: | 0.0001457 |
| inclination: | 97.7441° |
| perigee height: | 489 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 333.1406° |
| argument of perigee: | 198.6890° |
| revolutions per day: | 15.25310297 |
| mean anomaly at epoch: | 161.4294° |
| orbit number at epoch: | 95898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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