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 40912U 15049P 23087.64117697 .00049738 00000-0 13411-2 0 9999
2 40912 97.4260 104.1710 0010348 25.8091 114.3666 15.37593164417206
Epoch (UTC): | 28 March 2023 15:23:17 |
Eccentricity: | 0.0010348 |
inclination: | 97.4260° |
perigee height: | 446 km |
apogee height: | 460 km |
right ascension of ascending node: | 104.1710° |
argument of perigee: | 25.8091° |
revolutions per day: | 15.37593164 |
mean anomaly at epoch: | 114.3666° |
orbit number at epoch: | 41720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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