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 23079.67020454 .00010239 00000-0 90973-3 0 9993
2 40021 98.0485 40.9374 0010340 198.7649 161.3191 14.96294029475949
Epoch (UTC): | 20 March 2023 16:05:05 |
Eccentricity: | 0.0010340 |
inclination: | 98.0485° |
perigee height: | 571 km |
apogee height: | 585 km |
right ascension of ascending node: | 40.9374° |
argument of perigee: | 198.7649° |
revolutions per day: | 14.96294029 |
mean anomaly at epoch: | 161.3191° |
orbit number at epoch: | 47594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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