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 15332U 84105B 24276.92217765 .00003061 00000-0 35614-3 0 9994
2 15332 82.5356 215.9155 0019363 214.5073 210.0115 14.84889641140612
| Epoch (UTC): | 02 October 2024 22:07:56 |
| Eccentricity: | 0.0019363 |
| inclination: | 82.5356° |
| perigee height: | 600 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 215.9155° |
| argument of perigee: | 214.5073° |
| revolutions per day: | 14.84889641 |
| mean anomaly at epoch: | 210.0115° |
| orbit number at epoch: | 14061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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