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 12443U 81041B 24276.43856364 .00001180 00000-0 41894-3 0 9997
2 12443 74.0552 330.6855 0003354 141.8219 218.3171 14.35520710269862
Epoch (UTC): | 02 October 2024 10:31:31 |
Eccentricity: | 0.0003354 |
inclination: | 74.0552° |
perigee height: | 771 km |
apogee height: | 776 km |
right ascension of ascending node: | 330.6855° |
argument of perigee: | 141.8219° |
revolutions per day: | 14.35520710 |
mean anomaly at epoch: | 218.3171° |
orbit number at epoch: | 26986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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