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 39430U 13066Q 23342.13067993 .00001504 00000-0 26195-3 0 9993
2 39430 97.7565 223.0096 0143775 142.0545 219.0895 14.62854308534951
Epoch (UTC): | 08 December 2023 03:08:10 |
Eccentricity: | 0.0143775 |
inclination: | 97.7565° |
perigee height: | 582 km |
apogee height: | 785 km |
right ascension of ascending node: | 223.0096° |
argument of perigee: | 142.0545° |
revolutions per day: | 14.62854308 |
mean anomaly at epoch: | 219.0895° |
orbit number at epoch: | 53495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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