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 24311.80917725 .00000885 00000-0 30209-3 0 9995
2 27386 98.3031 268.0831 0001329 83.3653 334.5815 14.38748528189088
Epoch (UTC): | 06 November 2024 19:25:12 |
Eccentricity: | 0.0001329 |
inclination: | 98.3031° |
perigee height: | 761 km |
apogee height: | 763 km |
right ascension of ascending node: | 268.0831° |
argument of perigee: | 83.3653° |
revolutions per day: | 14.38748528 |
mean anomaly at epoch: | 334.5815° |
orbit number at epoch: | 18908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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