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 25343.50984768 .00014141 00000-0 26026-3 0 9994
2 25544 51.6310 158.4724 0003400 223.8185 136.2534 15.49447168542357
| Epoch (UTC): | 09 December 2025 12:14:10 |
| Eccentricity: | 0.0003400 |
| inclination: | 51.6310° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 158.4724° |
| argument of perigee: | 223.8185° |
| revolutions per day: | 15.49447168 |
| mean anomaly at epoch: | 136.2534° |
| orbit number at epoch: | 54235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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