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 39423U 13066H 24358.03705355 .00002575 00000-0 48748-3 0 9990
2 39423 97.6645 177.1757 0168165 135.5221 225.9623 14.56371072588120
Epoch (UTC): | 23 December 2024 00:53:21 |
Eccentricity: | 0.0168165 |
inclination: | 97.6645° |
perigee height: | 586 km |
apogee height: | 824 km |
right ascension of ascending node: | 177.1757° |
argument of perigee: | 135.5221° |
revolutions per day: | 14.56371072 |
mean anomaly at epoch: | 225.9623° |
orbit number at epoch: | 58812 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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