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 23333.64875986 .00003885 00000-0 66464-3 0 9995
2 39430 97.7563 215.0316 0143254 168.8719 191.5710 14.62808644533711
Epoch (UTC): | 29 November 2023 15:34:12 |
Eccentricity: | 0.0143254 |
inclination: | 97.7563° |
perigee height: | 583 km |
apogee height: | 785 km |
right ascension of ascending node: | 215.0316° |
argument of perigee: | 168.8719° |
revolutions per day: | 14.62808644 |
mean anomaly at epoch: | 191.5710° |
orbit number at epoch: | 53371 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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