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 24310.90664145 .00000769 00000-0 26414-3 0 9994
2 27386 98.3029 267.2097 0001334 83.8745 342.1068 14.38746134188954
Epoch (UTC): | 05 November 2024 21:45:33 |
Eccentricity: | 0.0001334 |
inclination: | 98.3029° |
perigee height: | 761 km |
apogee height: | 763 km |
right ascension of ascending node: | 267.2097° |
argument of perigee: | 83.8745° |
revolutions per day: | 14.38746134 |
mean anomaly at epoch: | 342.1068° |
orbit number at epoch: | 18895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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