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 65032U 26145.41570770 +.00000000 +00000-0 +51610-3 0 00004
2 65032 53.1589 298.0528 0001089 86.9397 273.1729 15.30212597 09
| Epoch (UTC): | 25 May 2026 09:58:37 |
| Eccentricity: | 0.0001089 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.0528° |
| argument of perigee: | 86.9397° |
| revolutions per day: | 15.30212597 |
| mean anomaly at epoch: | 273.1729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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