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 24753U 97012A 23088.51427993 .00000192 00000-0 11986-3 0 9991
2 24753 98.9195 129.0664 0008471 197.6860 162.4019 14.16094327342110
Epoch (UTC): | 29 March 2023 12:20:33 |
Eccentricity: | 0.0008471 |
inclination: | 98.9195° |
perigee height: | 832 km |
apogee height: | 845 km |
right ascension of ascending node: | 129.0664° |
argument of perigee: | 197.6860° |
revolutions per day: | 14.16094327 |
mean anomaly at epoch: | 162.4019° |
orbit number at epoch: | 34211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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