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 25200.53313927 .00000352 00000-0 37861-4 0 9993
2 15332 82.5354 304.3530 0019705 344.9691 26.0992 14.85521493204689
| Epoch (UTC): | 19 July 2025 12:47:43 |
| Eccentricity: | 0.0019705 |
| inclination: | 82.5354° |
| perigee height: | 598 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 304.3530° |
| argument of perigee: | 344.9691° |
| revolutions per day: | 14.85521493 |
| mean anomaly at epoch: | 26.0992° |
| orbit number at epoch: | 20468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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