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 23318U 94066B 24278.86035641 .00002429 00000-0 31585-3 0 9990
2 23318 82.5427 214.6252 0024225 139.6122 220.6896 14.80103978616555
Epoch (UTC): | 04 October 2024 20:38:54 |
Eccentricity: | 0.0024225 |
inclination: | 82.5427° |
perigee height: | 612 km |
apogee height: | 646 km |
right ascension of ascending node: | 214.6252° |
argument of perigee: | 139.6122° |
revolutions per day: | 14.80103978 |
mean anomaly at epoch: | 220.6896° |
orbit number at epoch: | 61655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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