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 40021U 14033M 24259.21423044 .00026109 00000-0 15476-2 0 9993
2 40021 98.0966 247.9339 0014339 144.6212 215.5971 15.11273721557708
Epoch (UTC): | 15 September 2024 05:08:29 |
Eccentricity: | 0.0014339 |
inclination: | 98.0966° |
perigee height: | 522 km |
apogee height: | 542 km |
right ascension of ascending node: | 247.9339° |
argument of perigee: | 144.6212° |
revolutions per day: | 15.11273721 |
mean anomaly at epoch: | 215.5971° |
orbit number at epoch: | 55770 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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