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 22175.75016203 .00006668 00000-0 23546-3 0 9991
2 43137 97.3688 250.8407 0006722 348.1329 11.9752 15.29527982247462
Epoch (UTC): | 24 June 2022 18:00:13 |
Eccentricity: | 0.0006722 |
inclination: | 97.3688° |
perigee height: | 472 km |
apogee height: | 482 km |
right ascension of ascending node: | 250.8407° |
argument of perigee: | 348.1329° |
revolutions per day: | 15.29527982 |
mean anomaly at epoch: | 11.9752° |
orbit number at epoch: | 24746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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