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 23150.45178480 .00000190 00000-0 75724-4 0 9995
2 12443 74.0520 149.9234 0003154 64.5527 295.5952 14.35036760199425
Epoch (UTC): | 30 May 2023 10:50:34 |
Eccentricity: | 0.0003154 |
inclination: | 74.0520° |
perigee height: | 772 km |
apogee height: | 777 km |
right ascension of ascending node: | 149.9234° |
argument of perigee: | 64.5527° |
revolutions per day: | 14.35036760 |
mean anomaly at epoch: | 295.5952° |
orbit number at epoch: | 19942 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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