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 40012U 14033C 23089.24602754 .00004452 00000-0 63381-3 0 9999
2 40012 97.6686 267.2293 0055068 313.3286 46.3340 14.76265965472129
Epoch (UTC): | 30 March 2023 05:54:16 |
Eccentricity: | 0.0055068 |
inclination: | 97.6686° |
perigee height: | 602 km |
apogee height: | 680 km |
right ascension of ascending node: | 267.2293° |
argument of perigee: | 313.3286° |
revolutions per day: | 14.76265965 |
mean anomaly at epoch: | 46.3340° |
orbit number at epoch: | 47212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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