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 27386U 02009A 24319.17183066 .00000490 00000-0 17322-3 0 9999
2 27386 98.3046 275.2089 0001365 82.6150 288.1846 14.38758475190142
Epoch (UTC): | 14 November 2024 04:07:26 |
Eccentricity: | 0.0001365 |
inclination: | 98.3046° |
perigee height: | 761 km |
apogee height: | 763 km |
right ascension of ascending node: | 275.2089° |
argument of perigee: | 82.6150° |
revolutions per day: | 14.38758475 |
mean anomaly at epoch: | 288.1846° |
orbit number at epoch: | 19014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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