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 43017U 17073E 25073.62681041 .00016311 00000-0 85923-3 0 9990
2 43017 97.5418 306.6469 0181789 102.2858 259.8787 15.02452226396143
Epoch (UTC): | 14 March 2025 15:02:36 |
Eccentricity: | 0.0181789 |
inclination: | 97.5418° |
perigee height: | 433 km |
apogee height: | 685 km |
right ascension of ascending node: | 306.6469° |
argument of perigee: | 102.2858° |
revolutions per day: | 15.02452226 |
mean anomaly at epoch: | 259.8787° |
orbit number at epoch: | 39614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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