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 24260.93565726 .00029034 00000-0 17154-2 0 9993
2 40021 98.0964 249.7566 0014462 139.9289 220.3009 15.11364721557961
Epoch (UTC): | 16 September 2024 22:27:20 |
Eccentricity: | 0.0014462 |
inclination: | 98.0964° |
perigee height: | 522 km |
apogee height: | 542 km |
right ascension of ascending node: | 249.7566° |
argument of perigee: | 139.9289° |
revolutions per day: | 15.11364721 |
mean anomaly at epoch: | 220.3009° |
orbit number at epoch: | 55796 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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