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 25544U 98067A 25341.89741187 .00012051 00000-0 22339-3 0 9991
2 25544 51.6302 166.4547 0003425 217.7386 142.3363 15.49404055542101
| Epoch (UTC): | 07 December 2025 21:32:16 |
| Eccentricity: | 0.0003425 |
| inclination: | 51.6302° |
| perigee height: | 416 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 166.4547° |
| argument of perigee: | 217.7386° |
| revolutions per day: | 15.49404055 |
| mean anomaly at epoch: | 142.3363° |
| orbit number at epoch: | 54210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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