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 23827U 96017A 24283.82685099 .00001043 00000-0 48067-3 0 9997
2 23827 99.0415 279.3288 0002260 262.7422 97.3498 14.23343847482313
Epoch (UTC): | 09 October 2024 19:50:39 |
Eccentricity: | 0.0002260 |
inclination: | 99.0415° |
perigee height: | 812 km |
apogee height: | 815 km |
right ascension of ascending node: | 279.3288° |
argument of perigee: | 262.7422° |
revolutions per day: | 14.23343847 |
mean anomaly at epoch: | 97.3498° |
orbit number at epoch: | 48231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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