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 27939U 03042A 24310.62965569 .00005368 00000-0 88053-3 0 9996
2 27939 98.3070 109.3247 0011310 338.6056 159.9328 14.71089816128937
Epoch (UTC): | 05 November 2024 15:06:42 |
Eccentricity: | 0.0011310 |
inclination: | 98.3070° |
perigee height: | 649 km |
apogee height: | 665 km |
right ascension of ascending node: | 109.3247° |
argument of perigee: | 338.6056° |
revolutions per day: | 14.71089816 |
mean anomaly at epoch: | 159.9328° |
orbit number at epoch: | 12893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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