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 22177.38857024 .00002841 00000-0 27919-3 0 9990
2 40021 98.0123 127.7515 0013039 18.3840 341.7847 14.92923697436032
Epoch (UTC): | 26 June 2022 09:19:32 |
Eccentricity: | 0.0013039 |
inclination: | 98.0123° |
perigee height: | 580 km |
apogee height: | 598 km |
right ascension of ascending node: | 127.7515° |
argument of perigee: | 18.3840° |
revolutions per day: | 14.92923697 |
mean anomaly at epoch: | 341.7847° |
orbit number at epoch: | 43603 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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