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 14780U 84021A 25197.71379678 .00001151 00000-0 87639-4 0 9992
2 14780 98.0846 97.6059 0073209 158.8324 201.5956 15.02207347740982
Epoch (UTC): | 16 July 2025 17:07:52 |
Eccentricity: | 0.0073209 |
inclination: | 98.0846° |
perigee height: | 509 km |
apogee height: | 611 km |
right ascension of ascending node: | 97.6059° |
argument of perigee: | 158.8324° |
revolutions per day: | 15.02207347 |
mean anomaly at epoch: | 201.5956° |
orbit number at epoch: | 74098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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