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 25198.31329003 .00001263 00000-0 95642-4 0 9993
2 14780 98.0845 98.2307 0073268 156.8281 203.6274 15.02209658741073
Epoch (UTC): | 17 July 2025 07:31:08 |
Eccentricity: | 0.0073268 |
inclination: | 98.0845° |
perigee height: | 509 km |
apogee height: | 611 km |
right ascension of ascending node: | 98.2307° |
argument of perigee: | 156.8281° |
revolutions per day: | 15.02209658 |
mean anomaly at epoch: | 203.6274° |
orbit number at epoch: | 74107 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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