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 23259U 90081CQ 24357.94886995 .00003290 00000-0 12401-2 0 9992
2 23259 98.5330 352.5855 0018169 150.0008 210.2221 14.31976365732673
Epoch (UTC): | 22 December 2024 22:46:22 |
Eccentricity: | 0.0018169 |
inclination: | 98.5330° |
perigee height: | 772 km |
apogee height: | 798 km |
right ascension of ascending node: | 352.5855° |
argument of perigee: | 150.0008° |
revolutions per day: | 14.31976365 |
mean anomaly at epoch: | 210.2221° |
orbit number at epoch: | 73267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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