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 is defined by the following mean orbital elements,
1 15427U 26088.06279733 +.00000000 +00000-0 +82306-4 0 00006
2 15427 99.1073 112.8165 0014115 213.5010 205.1188 14.17045254 06
| Epoch (UTC): | 29 March 2026 01:30:25 |
| Eccentricity: | 0.0014115 |
| inclination: | 99.1073° |
| perigee height: | 825 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 112.8165° |
| argument of perigee: | 213.5010° |
| revolutions per day: | 14.17045254 |
| mean anomaly at epoch: | 205.1188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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