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 41339U 16012C 24260.14807939 .00010036 00000-0 60831-3 0 9996
2 41339 31.0070 163.8325 0010158 70.4192 289.7542 15.09268062471322
Epoch (UTC): | 16 September 2024 03:33:14 |
Eccentricity: | 0.0010158 |
inclination: | 31.0070° |
perigee height: | 531 km |
apogee height: | 545 km |
right ascension of ascending node: | 163.8325° |
argument of perigee: | 70.4192° |
revolutions per day: | 15.09268062 |
mean anomaly at epoch: | 289.7542° |
orbit number at epoch: | 47132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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