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 19316U 76077FK 24352.39224525 -.00000001 00000-0 45499-3 0 9991
2 19316 102.0824 151.7013 0210518 281.4641 103.5111 12.03642759746233
Epoch (UTC): | 17 December 2024 09:24:49 |
Eccentricity: | 0.0210518 |
inclination: | 102.0824° |
perigee height: | 1495 km |
apogee height: | 1834 km |
right ascension of ascending node: | 151.7013° |
argument of perigee: | 281.4641° |
revolutions per day: | 12.03642759 |
mean anomaly at epoch: | 103.5111° |
orbit number at epoch: | 74623 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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