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 37766U 11039B 25199.17925551 .00000447 00000-0 82678-4 0 9994
2 37766 98.1378 93.4043 0041882 292.3444 67.3325 14.69731810747757
| Epoch (UTC): | 18 July 2025 04:18:07 |
| Eccentricity: | 0.0041882 |
| inclination: | 98.1378° |
| perigee height: | 632 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 93.4043° |
| argument of perigee: | 292.3444° |
| revolutions per day: | 14.69731810 |
| mean anomaly at epoch: | 67.3325° |
| orbit number at epoch: | 74775 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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