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 23340.15431854 .00002241 00000-0 33846-3 0 9996
2 39161 97.8546 47.4667 0010150 131.6916 228.5164 14.75212559568478
Epoch (UTC): | 06 December 2023 03:42:13 |
Eccentricity: | 0.0010150 |
inclination: | 97.8546° |
perigee height: | 637 km |
apogee height: | 651 km |
right ascension of ascending node: | 47.4667° |
argument of perigee: | 131.6916° |
revolutions per day: | 14.75212559 |
mean anomaly at epoch: | 228.5164° |
orbit number at epoch: | 56847 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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