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 47592U 26145.66668980 +.00000000 +00000-0 +53698-3 0 00001
2 47592 53.0327 337.2041 0004775 277.0975 251.2931 15.84947173 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0004775 |
| inclination: | 53.0327° |
| perigee height: | 313 km |
| apogee height: | 320 km |
| right ascension of ascending node: | 337.2041° |
| argument of perigee: | 277.0975° |
| revolutions per day: | 15.84947173 |
| mean anomaly at epoch: | 251.2931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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