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 23331.90309022 .00005422 00000-0 74139-3 0 9995
2 40012 97.6817 138.1482 0053429 243.6996 115.8721 14.77949674507944
Epoch (UTC): | 27 November 2023 21:40:26 |
Eccentricity: | 0.0053429 |
inclination: | 97.6817° |
perigee height: | 598 km |
apogee height: | 673 km |
right ascension of ascending node: | 138.1482° |
argument of perigee: | 243.6996° |
revolutions per day: | 14.77949674 |
mean anomaly at epoch: | 115.8721° |
orbit number at epoch: | 50794 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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