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 23265.16631977 .00064890 00000-0 96673-3 0 9990
2 43137 97.3181 345.9259 0005047 146.7221 213.4351 15.54883437317339
Epoch (UTC): | 22 September 2023 03:59:30 |
Eccentricity: | 0.0005047 |
inclination: | 97.3181° |
perigee height: | 399 km |
apogee height: | 406 km |
right ascension of ascending node: | 345.9259° |
argument of perigee: | 146.7221° |
revolutions per day: | 15.54883437 |
mean anomaly at epoch: | 213.4351° |
orbit number at epoch: | 31733 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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