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 30947U 99025BAM 24358.09387504 .00001847 00000-0 60449-3 0 9992
2 30947 98.8528 232.1451 0097434 215.3133 144.1574 14.37095817933970
Epoch (UTC): | 23 December 2024 02:15:10 |
Eccentricity: | 0.0097434 |
inclination: | 98.8528° |
perigee height: | 698 km |
apogee height: | 838 km |
right ascension of ascending node: | 232.1451° |
argument of perigee: | 215.3133° |
revolutions per day: | 14.37095817 |
mean anomaly at epoch: | 144.1574° |
orbit number at epoch: | 93397 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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