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 30791U 99057PA 24358.05943090 .00008308 00000-0 17204-2 0 9997
2 30791 98.5885 29.0974 0004702 203.7767 185.4737 14.60514743939631
Epoch (UTC): | 23 December 2024 01:25:34 |
Eccentricity: | 0.0004702 |
inclination: | 98.5885° |
perigee height: | 688 km |
apogee height: | 695 km |
right ascension of ascending node: | 29.0974° |
argument of perigee: | 203.7767° |
revolutions per day: | 14.60514743 |
mean anomaly at epoch: | 185.4737° |
orbit number at epoch: | 93963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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