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 65560U 26144.97646904 +.00000000 +00000-0 +17124-3 0 00005
2 65560 49.9861 146.5397 0009105 255.2543 104.7386 14.84078443 09
| Epoch (UTC): | 24 May 2026 23:26:06 |
| Eccentricity: | 0.0009105 |
| inclination: | 49.9861° |
| perigee height: | 610 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 146.5397° |
| argument of perigee: | 255.2543° |
| revolutions per day: | 14.84078443 |
| mean anomaly at epoch: | 104.7386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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