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 23339.89400312 .00004691 00000-0 44349-3 0 9990
2 32785 97.7297 302.5840 0009985 251.5136 108.5000 14.94123396846514
Epoch (UTC): | 05 December 2023 21:27:21 |
Eccentricity: | 0.0009985 |
inclination: | 97.7297° |
perigee height: | 578 km |
apogee height: | 592 km |
right ascension of ascending node: | 302.5840° |
argument of perigee: | 251.5136° |
revolutions per day: | 14.94123396 |
mean anomaly at epoch: | 108.5000° |
orbit number at epoch: | 84651 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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