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 24308.88845219 .00000950 00000-0 32326-3 0 9992
2 27386 98.3024 265.2566 0001325 84.6963 334.1733 14.38743052188595
Epoch (UTC): | 03 November 2024 21:19:22 |
Eccentricity: | 0.0001325 |
inclination: | 98.3024° |
perigee height: | 762 km |
apogee height: | 763 km |
right ascension of ascending node: | 265.2566° |
argument of perigee: | 84.6963° |
revolutions per day: | 14.38743052 |
mean anomaly at epoch: | 334.1733° |
orbit number at epoch: | 18859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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