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 31133U 07012R 24357.83217113 .00002780 00000-0 51656-3 0 9991
2 31133 98.3723 319.3048 0073216 216.6890 142.9287 14.64295570941060
Epoch (UTC): | 22 December 2024 19:58:19 |
Eccentricity: | 0.0073216 |
inclination: | 98.3723° |
perigee height: | 627 km |
apogee height: | 731 km |
right ascension of ascending node: | 319.3048° |
argument of perigee: | 216.6890° |
revolutions per day: | 14.64295570 |
mean anomaly at epoch: | 142.9287° |
orbit number at epoch: | 94106 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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