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 18025U 87043H 23088.07513355 .00021581 00000-0 13161-2 0 9999
2 18025 63.2949 340.8953 0934064 79.8555 290.6382 13.54790213190373
Epoch (UTC): | 29 March 2023 01:48:11 |
Eccentricity: | 0.0934064 |
inclination: | 63.2949° |
perigee height: | 360 km |
apogee height: | 1749 km |
right ascension of ascending node: | 340.8953° |
argument of perigee: | 79.8555° |
revolutions per day: | 13.54790213 |
mean anomaly at epoch: | 290.6382° |
orbit number at epoch: | 19037 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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