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 17974U 87041B 24258.87727728 .00000370 00000-0 20577-3 0 9991
2 17974 71.0064 92.9265 0015650 306.0816 149.5533 14.17487575931442
Epoch (UTC): | 14 September 2024 21:03:16 |
Eccentricity: | 0.0015650 |
inclination: | 71.0064° |
perigee height: | 822 km |
apogee height: | 845 km |
right ascension of ascending node: | 92.9265° |
argument of perigee: | 306.0816° |
revolutions per day: | 14.17487575 |
mean anomaly at epoch: | 149.5533° |
orbit number at epoch: | 93144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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