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 22142.11643858 .00006307 00000-0 63346-3 0 9999
2 40024 97.9830 85.3536 0013270 128.8687 231.3717 14.91571814430575
Epoch (UTC): | 22 May 2022 02:47:40 |
Eccentricity: | 0.0013270 |
inclination: | 97.9830° |
perigee height: | 584 km |
apogee height: | 602 km |
right ascension of ascending node: | 85.3536° |
argument of perigee: | 128.8687° |
revolutions per day: | 14.91571814 |
mean anomaly at epoch: | 231.3717° |
orbit number at epoch: | 43057 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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