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 32791U 08021J 23340.47972211 .00007352 00000-0 60126-3 0 9993
2 32791 97.6819 308.6178 0009485 177.1582 182.9697 14.99609521847539
| Epoch (UTC): | 06 December 2023 11:30:47 |
| Eccentricity: | 0.0009485 |
| inclination: | 97.6819° |
| perigee height: | 561 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 308.6178° |
| argument of perigee: | 177.1582° |
| revolutions per day: | 14.99609521 |
| mean anomaly at epoch: | 182.9697° |
| orbit number at epoch: | 84753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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