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 42847U 17042Y 23088.64994397 .00005241 00000-0 49192-3 0 9991
2 42847 97.3946 294.8230 0010279 115.4785 244.7501 14.94324104310855
Epoch (UTC): | 29 March 2023 15:35:55 |
Eccentricity: | 0.0010279 |
inclination: | 97.3946° |
perigee height: | 577 km |
apogee height: | 591 km |
right ascension of ascending node: | 294.8230° |
argument of perigee: | 115.4785° |
revolutions per day: | 14.94324104 |
mean anomaly at epoch: | 244.7501° |
orbit number at epoch: | 31085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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