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 65646U 26145.47210735 +.00000000 +00000-0 +65221-3 0 00006
2 65646 53.1585 310.6506 0001319 91.8473 268.2678 15.30214239 02
| Epoch (UTC): | 25 May 2026 11:19:50 |
| Eccentricity: | 0.0001319 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6506° |
| argument of perigee: | 91.8473° |
| revolutions per day: | 15.30214239 |
| mean anomaly at epoch: | 268.2678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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