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 32788U 08021F 23336.91662671 .00013779 00000-0 87896-3 0 9992
2 32788 97.5784 313.2600 0008740 123.5352 236.6713 15.08784855848600
Epoch (UTC): | 02 December 2023 21:59:56 |
Eccentricity: | 0.0008740 |
inclination: | 97.5784° |
perigee height: | 534 km |
apogee height: | 546 km |
right ascension of ascending node: | 313.2600° |
argument of perigee: | 123.5352° |
revolutions per day: | 15.08784855 |
mean anomaly at epoch: | 236.6713° |
orbit number at epoch: | 84860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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