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 24318.12859175 .00000506 00000-0 17859-3 0 9997
2 27386 98.3043 274.1991 0001345 82.7178 287.7301 14.38757244189993
Epoch (UTC): | 13 November 2024 03:05:10 |
Eccentricity: | 0.0001345 |
inclination: | 98.3043° |
perigee height: | 761 km |
apogee height: | 763 km |
right ascension of ascending node: | 274.1991° |
argument of perigee: | 82.7178° |
revolutions per day: | 14.38757244 |
mean anomaly at epoch: | 287.7301° |
orbit number at epoch: | 18999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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