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 32130U 99025CRY 24251.68643458 .00006792 00000-0 23056-2 0 9994
2 32130 98.8583 37.7450 0085636 247.4095 111.8012 14.34923260896154
Epoch (UTC): | 07 September 2024 16:28:27 |
Eccentricity: | 0.0085636 |
inclination: | 98.8583° |
perigee height: | 714 km |
apogee height: | 836 km |
right ascension of ascending node: | 37.7450° |
argument of perigee: | 247.4095° |
revolutions per day: | 14.34923260 |
mean anomaly at epoch: | 111.8012° |
orbit number at epoch: | 89615 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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