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 47559U 26145.66668980 +.00000000 +00000-0 +77902-3 0 00008
2 47559 53.0341 297.0372 0008171 258.3226 152.1740 15.88012516 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0008171 |
| inclination: | 53.0341° |
| perigee height: | 302 km |
| apogee height: | 313 km |
| right ascension of ascending node: | 297.0372° |
| argument of perigee: | 258.3226° |
| revolutions per day: | 15.88012516 |
| mean anomaly at epoch: | 152.1740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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