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 24262.45836229 .00023421 00000-0 13821-2 0 9992
2 40021 98.0973 251.3686 0014614 135.4974 224.7431 15.11455543558190
Epoch (UTC): | 18 September 2024 11:00:02 |
Eccentricity: | 0.0014614 |
inclination: | 98.0973° |
perigee height: | 521 km |
apogee height: | 542 km |
right ascension of ascending node: | 251.3686° |
argument of perigee: | 135.4974° |
revolutions per day: | 15.11455543 |
mean anomaly at epoch: | 224.7431° |
orbit number at epoch: | 55819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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