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 23335.76927265 .00004030 00000-0 68867-3 0 9990
2 39430 97.7560 217.0263 0143397 162.1529 198.4785 14.62824550534022
Epoch (UTC): | 01 December 2023 18:27:45 |
Eccentricity: | 0.0143397 |
inclination: | 97.7560° |
perigee height: | 583 km |
apogee height: | 785 km |
right ascension of ascending node: | 217.0263° |
argument of perigee: | 162.1529° |
revolutions per day: | 14.62824550 |
mean anomaly at epoch: | 198.4785° |
orbit number at epoch: | 53402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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