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 14552U 83122B 25348.28651289 .00000606 00000-0 66896-4 0 9997
2 14552 82.5238 49.9272 0016630 7.5427 352.6036 14.85756459248150
| Epoch (UTC): | 14 December 2025 06:52:34 |
| Eccentricity: | 0.0016630 |
| inclination: | 82.5238° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 49.9272° |
| argument of perigee: | 7.5427° |
| revolutions per day: | 14.85756459 |
| mean anomaly at epoch: | 352.6036° |
| orbit number at epoch: | 24815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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