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 14781U 84021B 25136.48179920 .00001442 00000-0 15778-3 0 9995
2 14781 97.7529 103.3311 0009280 61.8248 298.3905 14.89315372219058
Epoch (UTC): | 16 May 2025 11:33:47 |
Eccentricity: | 0.0009280 |
inclination: | 97.7529° |
perigee height: | 593 km |
apogee height: | 606 km |
right ascension of ascending node: | 103.3311° |
argument of perigee: | 61.8248° |
revolutions per day: | 14.89315372 |
mean anomaly at epoch: | 298.3905° |
orbit number at epoch: | 21905 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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