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 43137U 18004AC 23334.74225094 .00171139 00000-0 13698-2 0 9990
2 43137 97.3086 57.7842 0003565 244.1628 115.9267 15.70538337328187
Epoch (UTC): | 30 November 2023 17:48:50 |
Eccentricity: | 0.0003565 |
inclination: | 97.3086° |
perigee height: | 355 km |
apogee height: | 360 km |
right ascension of ascending node: | 57.7842° |
argument of perigee: | 244.1628° |
revolutions per day: | 15.70538337 |
mean anomaly at epoch: | 115.9267° |
orbit number at epoch: | 32818 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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