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 40024U 14033Q 23088.82860807 .00011132 00000-0 10275-2 0 9996
2 40024 98.0207 42.0713 0010782 173.7022 186.4335 14.94765370476558
Epoch (UTC): | 29 March 2023 19:53:11 |
Eccentricity: | 0.0010782 |
inclination: | 98.0207° |
perigee height: | 575 km |
apogee height: | 590 km |
right ascension of ascending node: | 42.0713° |
argument of perigee: | 173.7022° |
revolutions per day: | 14.94765370 |
mean anomaly at epoch: | 186.4335° |
orbit number at epoch: | 47655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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