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 54312U 22151BF 24358.01988265 .00006255 00000-0 25924-2 0 9999
2 54312 98.9263 26.2346 0022810 269.6097 90.2469 14.26771983109221
Epoch (UTC): | 23 December 2024 00:28:37 |
Eccentricity: | 0.0022810 |
inclination: | 98.9263° |
perigee height: | 786 km |
apogee height: | 819 km |
right ascension of ascending node: | 26.2346° |
argument of perigee: | 269.6097° |
revolutions per day: | 14.26771983 |
mean anomaly at epoch: | 90.2469° |
orbit number at epoch: | 10922 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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