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 5732U 71120B 25163.02746887 .00000205 00000-0 11512-3 0 9997
2 5732 81.2510 185.0960 0052023 120.8106 239.8198 14.06362120748829
Epoch (UTC): | 12 June 2025 00:39:33 |
Eccentricity: | 0.0052023 |
inclination: | 81.2510° |
perigee height: | 834 km |
apogee height: | 909 km |
right ascension of ascending node: | 185.0960° |
argument of perigee: | 120.8106° |
revolutions per day: | 14.06362120 |
mean anomaly at epoch: | 239.8198° |
orbit number at epoch: | 74882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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