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 13272U 82059B 24340.39699221 .00001608 00000-0 17887-3 0 9992
2 13272 82.5097 94.2227 0019328 102.6223 257.7156 14.86425341275693
Epoch (UTC): | 05 December 2024 09:31:40 |
Eccentricity: | 0.0019328 |
inclination: | 82.5097° |
perigee height: | 595 km |
apogee height: | 622 km |
right ascension of ascending node: | 94.2227° |
argument of perigee: | 102.6223° |
revolutions per day: | 14.86425341 |
mean anomaly at epoch: | 257.7156° |
orbit number at epoch: | 27569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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