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 35805U 97051SP 23333.14702315 .00032492 00000-0 76872-2 0 9992
2 35805 86.3109 25.5441 0074433 93.1044 267.8682 14.52233620747019
Epoch (UTC): | 29 November 2023 03:31:42 |
Eccentricity: | 0.0074433 |
inclination: | 86.3109° |
perigee height: | 665 km |
apogee height: | 771 km |
right ascension of ascending node: | 25.5441° |
argument of perigee: | 93.1044° |
revolutions per day: | 14.52233620 |
mean anomaly at epoch: | 267.8682° |
orbit number at epoch: | 74701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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