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 54686U 22167E 25322.50196803 .00014757 00000-0 53931-3 0 9991
2 54686 97.6675 118.3490 0009147 185.2488 174.8656 15.28159612163089
| Epoch (UTC): | 18 November 2025 12:02:50 |
| Eccentricity: | 0.0009147 |
| inclination: | 97.6675° |
| perigee height: | 475 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 118.3490° |
| argument of perigee: | 185.2488° |
| revolutions per day: | 15.28159612 |
| mean anomaly at epoch: | 174.8656° |
| orbit number at epoch: | 16308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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