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 39161U 13021C 24310.18039959 .00008741 00000-0 12182-2 0 9997
2 39161 97.8117 12.3571 0009802 128.7536 231.4553 14.77932964617903
Epoch (UTC): | 05 November 2024 04:19:46 |
Eccentricity: | 0.0009802 |
inclination: | 97.8117° |
perigee height: | 629 km |
apogee height: | 643 km |
right ascension of ascending node: | 12.3571° |
argument of perigee: | 128.7536° |
revolutions per day: | 14.77932964 |
mean anomaly at epoch: | 231.4553° |
orbit number at epoch: | 61790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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