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 12278U 78026DW 25161.93264505 .00002169 00000-0 64783-3 0 9991
2 12278 99.1179 321.1843 0038410 333.7439 185.3317 14.43676413289576
Epoch (UTC): | 10 June 2025 22:23:00 |
Eccentricity: | 0.0038410 |
inclination: | 99.1179° |
perigee height: | 719 km |
apogee height: | 774 km |
right ascension of ascending node: | 321.1843° |
argument of perigee: | 333.7439° |
revolutions per day: | 14.43676413 |
mean anomaly at epoch: | 185.3317° |
orbit number at epoch: | 28957 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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