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 31132U 07012Q 23333.84387294 .00004330 00000-0 84586-3 0 9993
2 31132 98.3198 285.9973 0077530 352.3965 7.6054 14.61535151884181
Epoch (UTC): | 29 November 2023 20:15:10 |
Eccentricity: | 0.0077530 |
inclination: | 98.3198° |
perigee height: | 633 km |
apogee height: | 743 km |
right ascension of ascending node: | 285.9973° |
argument of perigee: | 352.3965° |
revolutions per day: | 14.61535151 |
mean anomaly at epoch: | 7.6054° |
orbit number at epoch: | 88418 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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