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 65327U 26145.55666149 +.00000000 +00000-0 +28864-3 0 00007
2 65327 53.1589 209.8399 0001064 79.3422 280.7699 15.30204763 06
| Epoch (UTC): | 25 May 2026 13:21:35 |
| Eccentricity: | 0.0001064 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.8399° |
| argument of perigee: | 79.3422° |
| revolutions per day: | 15.30204763 |
| mean anomaly at epoch: | 280.7699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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