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 00047U 60007C 24311.95881605 .00001975 00000-0 44509-3 0 9994
2 00047 66.6651 183.6199 0226270 210.7908 147.9765 14.44071634365979
Epoch (UTC): | 06 November 2024 23:00:41 |
Eccentricity: | 0.0226270 |
inclination: | 66.6651° |
perigee height: | 584 km |
apogee height: | 906 km |
right ascension of ascending node: | 183.6199° |
argument of perigee: | 210.7908° |
revolutions per day: | 14.44071634 |
mean anomaly at epoch: | 147.9765° |
orbit number at epoch: | 36597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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