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 24261.20944516 .00056917 00000-0 37769-2 0 9991
2 32791 97.6989 232.0778 0005438 30.3477 329.8064 15.06998665890447
| Epoch (UTC): | 17 September 2024 05:01:36 |
| Eccentricity: | 0.0005438 |
| inclination: | 97.6989° |
| perigee height: | 541 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 232.0778° |
| argument of perigee: | 30.3477° |
| revolutions per day: | 15.06998665 |
| mean anomaly at epoch: | 329.8064° |
| orbit number at epoch: | 89044 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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