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 13154U 82039B 23338.08729981 .00003977 00000-0 29439-3 0 9995
2 13154 81.1825 81.4667 0037508 154.4783 205.8301 15.02380801257469
Epoch (UTC): | 04 December 2023 02:05:42 |
Eccentricity: | 0.0037508 |
inclination: | 81.1825° |
perigee height: | 533 km |
apogee height: | 585 km |
right ascension of ascending node: | 81.4667° |
argument of perigee: | 154.4783° |
revolutions per day: | 15.02380801 |
mean anomaly at epoch: | 205.8301° |
orbit number at epoch: | 25746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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