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 23332.47221070 .00011622 00000-0 95169-3 0 9994
2 32791 97.6791 300.7207 0008614 204.8751 155.2058 14.99426462846335
| Epoch (UTC): | 28 November 2023 11:19:59 |
| Eccentricity: | 0.0008614 |
| inclination: | 97.6791° |
| perigee height: | 562 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.7207° |
| argument of perigee: | 204.8751° |
| revolutions per day: | 14.99426462 |
| mean anomaly at epoch: | 155.2058° |
| orbit number at epoch: | 84633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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