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 15427U 84123A 25131.80081632 .00000160 00000-0 10271-3 0 9998
2 15427 99.1226 143.5361 0015464 49.5173 123.1843 14.16915240 86573
Epoch (UTC): | 11 May 2025 19:13:10 |
Eccentricity: | 0.0015464 |
inclination: | 99.1226° |
perigee height: | 824 km |
apogee height: | 847 km |
right ascension of ascending node: | 143.5361° |
argument of perigee: | 49.5173° |
revolutions per day: | 14.16915240 |
mean anomaly at epoch: | 123.1843° |
orbit number at epoch: | 8657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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