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 15427U 84123A 25347.99657444 .00000166 00000-0 10560-3 0 9994
2 15427 99.1151 5.1973 0015108 151.5145 271.1473 14.17003608117193
| Epoch (UTC): | 13 December 2025 23:55:04 |
| Eccentricity: | 0.0015108 |
| inclination: | 99.1151° |
| perigee height: | 824 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 5.1973° |
| argument of perigee: | 151.5145° |
| revolutions per day: | 14.17003608 |
| mean anomaly at epoch: | 271.1473° |
| orbit number at epoch: | 11719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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