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 00050U 60009B 25193.88793587 -.00000053 00000-0 31607-3 0 9994
2 00050 47.2294 134.8893 0112971 83.3720 277.9913 12.20156676896271
Epoch (UTC): | 12 July 2025 21:18:37 |
Eccentricity: | 0.0112971 |
inclination: | 47.2294° |
perigee height: | 1502 km |
apogee height: | 1682 km |
right ascension of ascending node: | 134.8893° |
argument of perigee: | 83.3720° |
revolutions per day: | 12.20156676 |
mean anomaly at epoch: | 277.9913° |
orbit number at epoch: | 89627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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