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 40907U 15049J 24259.92682776 .00164897 00000-0 15787-2 0 9993
2 40907 97.4639 283.4326 0001164 331.1083 29.0112 15.66152779498813
Epoch (UTC): | 15 September 2024 22:14:37 |
Eccentricity: | 0.0001164 |
inclination: | 97.4639° |
perigee height: | 369 km |
apogee height: | 371 km |
right ascension of ascending node: | 283.4326° |
argument of perigee: | 331.1083° |
revolutions per day: | 15.66152779 |
mean anomaly at epoch: | 29.0112° |
orbit number at epoch: | 49881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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