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 23342.50103178 .00150517 00000-0 10237-2 0 9998
2 40912 97.3930 6.3891 0005857 130.3269 229.8508 15.74447795456692
Epoch (UTC): | 08 December 2023 12:01:29 |
Eccentricity: | 0.0005857 |
inclination: | 97.3930° |
perigee height: | 342 km |
apogee height: | 350 km |
right ascension of ascending node: | 6.3891° |
argument of perigee: | 130.3269° |
revolutions per day: | 15.74447795 |
mean anomaly at epoch: | 229.8508° |
orbit number at epoch: | 45669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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