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 47587U 26145.66668980 +.00000000 +00000-0 +82826-3 0 00000
2 47587 53.0374 308.7093 0005700 279.5156 65.6702 15.87408082 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0005700 |
| inclination: | 53.0374° |
| perigee height: | 306 km |
| apogee height: | 313 km |
| right ascension of ascending node: | 308.7093° |
| argument of perigee: | 279.5156° |
| revolutions per day: | 15.87408082 |
| mean anomaly at epoch: | 65.6702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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