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 32785U 08021C 24318.15316066 .00009516 00000-0 76327-3 0 9991
2 32785 97.7719 282.7161 0010539 188.8616 171.2423 15.00268824897853
Epoch (UTC): | 13 November 2024 03:40:33 |
Eccentricity: | 0.0010539 |
inclination: | 97.7719° |
perigee height: | 559 km |
apogee height: | 573 km |
right ascension of ascending node: | 282.7161° |
argument of perigee: | 188.8616° |
revolutions per day: | 15.00268824 |
mean anomaly at epoch: | 171.2423° |
orbit number at epoch: | 89785 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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