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 40011U 14033B 24280.84911396 .00007331 00000-0 85932-3 0 9998
2 40011 97.5693 125.0258 0024523 188.5114 171.5689 14.85053234556934
Epoch (UTC): | 06 October 2024 20:22:43 |
Eccentricity: | 0.0024523 |
inclination: | 97.5693° |
perigee height: | 596 km |
apogee height: | 630 km |
right ascension of ascending node: | 125.0258° |
argument of perigee: | 188.5114° |
revolutions per day: | 14.85053234 |
mean anomaly at epoch: | 171.5689° |
orbit number at epoch: | 55693 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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