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 23155.90700931 .00009090 00000-0 66749-3 0 9997
2 32788 97.5577 135.6024 0009208 46.1390 314.0595 15.03646656821261
Epoch (UTC): | 04 June 2023 21:46:05 |
Eccentricity: | 0.0009208 |
inclination: | 97.5577° |
perigee height: | 549 km |
apogee height: | 562 km |
right ascension of ascending node: | 135.6024° |
argument of perigee: | 46.1390° |
revolutions per day: | 15.03646656 |
mean anomaly at epoch: | 314.0595° |
orbit number at epoch: | 82126 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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