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 65356U 26145.45386814 +.00000000 +00000-0 +48407-3 0 00001
2 65356 53.1577 171.9348 0001274 79.9766 280.1379 15.30201783 06
| Epoch (UTC): | 25 May 2026 10:53:34 |
| Eccentricity: | 0.0001274 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.9348° |
| argument of perigee: | 79.9766° |
| revolutions per day: | 15.30201783 |
| mean anomaly at epoch: | 280.1379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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