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 13066U 82012B 24316.36393869 .00000165 00000-0 14997-3 0 9997
2 13066 82.8985 356.6774 0042558 229.8140 140.3309 13.77319199147176
Epoch (UTC): | 11 November 2024 08:44:04 |
Eccentricity: | 0.0042558 |
inclination: | 82.8985° |
perigee height: | 942 km |
apogee height: | 1004 km |
right ascension of ascending node: | 356.6774° |
argument of perigee: | 229.8140° |
revolutions per day: | 13.77319199 |
mean anomaly at epoch: | 140.3309° |
orbit number at epoch: | 14717 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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