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 30139U 99025SU 24280.62489425 .00006122 00000-0 37757-2 0 9999
2 30139 98.4081 152.0168 0136985 71.6560 350.4733 14.01181935901927
Epoch (UTC): | 06 October 2024 14:59:50 |
Eccentricity: | 0.0136985 |
inclination: | 98.4081° |
perigee height: | 790 km |
apogee height: | 989 km |
right ascension of ascending node: | 152.0168° |
argument of perigee: | 71.6560° |
revolutions per day: | 14.01181935 |
mean anomaly at epoch: | 350.4733° |
orbit number at epoch: | 90192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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