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 25135.34190934 .00008105 00000-0 15227-3 0 9993
2 25544 51.6360 109.7771 0002557 112.3430 38.3717 15.49538266510068
| Epoch (UTC): | 15 May 2025 08:12:20 |
| Eccentricity: | 0.0002557 |
| inclination: | 51.6360° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 109.7771° |
| argument of perigee: | 112.3430° |
| revolutions per day: | 15.49538266 |
| mean anomaly at epoch: | 38.3717° |
| orbit number at epoch: | 51006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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