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 23088.92542459 .00043301 00000-0 11657-2 0 9999
2 40912 97.4260 105.4697 0010159 24.0948 20.2852 15.37677067417405
Epoch (UTC): | 29 March 2023 22:12:36 |
Eccentricity: | 0.0010159 |
inclination: | 97.4260° |
perigee height: | 446 km |
apogee height: | 460 km |
right ascension of ascending node: | 105.4697° |
argument of perigee: | 24.0948° |
revolutions per day: | 15.37677067 |
mean anomaly at epoch: | 20.2852° |
orbit number at epoch: | 41740 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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