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 40908U 15049K 24261.16586210 .00035633 00000-0 12551-2 0 9990
2 40908 97.5243 270.7005 0012592 37.1731 323.0378 15.29140813497533
Epoch (UTC): | 17 September 2024 03:58:50 |
Eccentricity: | 0.0012592 |
inclination: | 97.5243° |
perigee height: | 470 km |
apogee height: | 487 km |
right ascension of ascending node: | 270.7005° |
argument of perigee: | 37.1731° |
revolutions per day: | 15.29140813 |
mean anomaly at epoch: | 323.0378° |
orbit number at epoch: | 49753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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