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 37839U 11058B 24263.53054692 .00000859 00000-0 31066-3 0 9997
2 37839 19.9597 209.2142 0018550 257.4471 260.7172 14.13323658669081
Epoch (UTC): | 19 September 2024 12:43:59 |
Eccentricity: | 0.0018550 |
inclination: | 19.9597° |
perigee height: | 834 km |
apogee height: | 861 km |
right ascension of ascending node: | 209.2142° |
argument of perigee: | 257.4471° |
revolutions per day: | 14.13323658 |
mean anomaly at epoch: | 260.7172° |
orbit number at epoch: | 66908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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