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 39439U 13066Z 23335.82654308 .00018778 00000-0 17355-2 0 9990
2 39439 97.7021 297.1896 0054715 80.0076 280.7313 14.93468206542302
Epoch (UTC): | 01 December 2023 19:50:13 |
Eccentricity: | 0.0054715 |
inclination: | 97.7021° |
perigee height: | 549 km |
apogee height: | 625 km |
right ascension of ascending node: | 297.1896° |
argument of perigee: | 80.0076° |
revolutions per day: | 14.93468206 |
mean anomaly at epoch: | 280.7313° |
orbit number at epoch: | 54230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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