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 43897U 18111X 24261.16905111 .00059081 00000-0 12700-2 0 9997
2 43897 97.0625 126.4742 0014962 22.6439 337.5468 15.44348635319277
Epoch (UTC): | 17 September 2024 04:03:26 |
Eccentricity: | 0.0014962 |
inclination: | 97.0625° |
perigee height: | 423 km |
apogee height: | 443 km |
right ascension of ascending node: | 126.4742° |
argument of perigee: | 22.6439° |
revolutions per day: | 15.44348635 |
mean anomaly at epoch: | 337.5468° |
orbit number at epoch: | 31927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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