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 24310.58346286 .00007643 00000-0 12272-2 0 9993
2 39430 97.7072 176.3741 0136699 162.0900 198.5191 14.65781620583565
Epoch (UTC): | 05 November 2024 14:00:11 |
Eccentricity: | 0.0136699 |
inclination: | 97.7072° |
perigee height: | 578 km |
apogee height: | 771 km |
right ascension of ascending node: | 176.3741° |
argument of perigee: | 162.0900° |
revolutions per day: | 14.65781620 |
mean anomaly at epoch: | 198.5191° |
orbit number at epoch: | 58356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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