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 15595U 85021A 24260.73711465 .00001233 00000-0 44065-3 0 9990
2 15595 108.0519 192.8218 0001190 285.0738 75.0272 14.39187449 70882
| Epoch (UTC): | 16 September 2024 17:41:26 |
| Eccentricity: | 0.0001190 |
| inclination: | 108.0519° |
| perigee height: | 760 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 192.8218° |
| argument of perigee: | 285.0738° |
| revolutions per day: | 14.39187449 |
| mean anomaly at epoch: | 75.0272° |
| orbit number at epoch: | 7088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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