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 41590U 16038C 24276.87158250 .00000147 00000-0 36481-2 0 9990
2 41590 21.8588 100.1964 7931821 67.6335 354.4184 1.44379436 36846
Epoch (UTC): | 02 October 2024 20:55:04 |
Eccentricity: | 0.7931821 |
inclination: | 21.8588° |
perigee height: | 461 km |
apogee height: | 52917 km |
right ascension of ascending node: | 100.1964° |
argument of perigee: | 67.6335° |
revolutions per day: | 1.44379436 |
mean anomaly at epoch: | 354.4184° |
orbit number at epoch: | 3684 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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