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 40958U 15057A 24284.86791635 .00005635 00000-0 83716-3 0 9996
2 40958 97.6652 298.9468 0019087 104.6945 255.6382 14.75245318484662
Epoch (UTC): | 10 October 2024 20:49:47 |
Eccentricity: | 0.0019087 |
inclination: | 97.6652° |
perigee height: | 631 km |
apogee height: | 658 km |
right ascension of ascending node: | 298.9468° |
argument of perigee: | 104.6945° |
revolutions per day: | 14.75245318 |
mean anomaly at epoch: | 255.6382° |
orbit number at epoch: | 48466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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