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 15360U 84109B 25198.52036541 .00000134 00000-0 11867-3 0 9992
2 15360 82.9394 14.3416 0042636 74.5184 286.0676 13.77017085 47589
Epoch (UTC): | 17 July 2025 12:29:19 |
Eccentricity: | 0.0042636 |
inclination: | 82.9394° |
perigee height: | 943 km |
apogee height: | 1006 km |
right ascension of ascending node: | 14.3416° |
argument of perigee: | 74.5184° |
revolutions per day: | 13.77017085 |
mean anomaly at epoch: | 286.0676° |
orbit number at epoch: | 4758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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