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 32787U 08021E 23273.89547104 .00015242 00000-0 11242-2 0 9999
2 32787 97.5922 248.1084 0013137 20.5363 339.6388 15.03311940838572
Epoch (UTC): | 30 September 2023 21:29:28 |
Eccentricity: | 0.0013137 |
inclination: | 97.5922° |
perigee height: | 547 km |
apogee height: | 566 km |
right ascension of ascending node: | 248.1084° |
argument of perigee: | 20.5363° |
revolutions per day: | 15.03311940 |
mean anomaly at epoch: | 339.6388° |
orbit number at epoch: | 83857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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