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 65823U 26145.27183059 +.00000000 +00000-0 +54924-3 0 00007
2 65823 53.1572 92.9714 0001126 88.7550 271.3580 15.30210849 03
| Epoch (UTC): | 25 May 2026 06:31:26 |
| Eccentricity: | 0.0001126 |
| inclination: | 53.1572° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 92.9714° |
| argument of perigee: | 88.7550° |
| revolutions per day: | 15.30210849 |
| mean anomaly at epoch: | 271.3580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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