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 25197.73223905 .00006509 00000-0 11952-3 0 9996
2 25544 51.6367 160.6113 0002844 25.5140 36.8267 15.50574159519743
| Epoch (UTC): | 16 July 2025 17:34:25 |
| Eccentricity: | 0.0002844 |
| inclination: | 51.6367° |
| perigee height: | 413 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 160.6113° |
| argument of perigee: | 25.5140° |
| revolutions per day: | 15.50574159 |
| mean anomaly at epoch: | 36.8267° |
| orbit number at epoch: | 51974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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