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 23085.88905821 .00010749 00000-0 95053-3 0 9993
2 40021 98.0498 47.3325 0011247 177.0619 183.0670 14.96458194476875
Epoch (UTC): | 26 March 2023 21:20:14 |
Eccentricity: | 0.0011247 |
inclination: | 98.0498° |
perigee height: | 570 km |
apogee height: | 585 km |
right ascension of ascending node: | 47.3325° |
argument of perigee: | 177.0619° |
revolutions per day: | 14.96458194 |
mean anomaly at epoch: | 183.0670° |
orbit number at epoch: | 47687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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