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 65126U 26145.60212359 +.00000000 +00000-0 +18458-3 0 00008
2 65126 49.9657 231.8419 0021327 254.4304 105.4279 14.82076915 08
| Epoch (UTC): | 25 May 2026 14:27:03 |
| Eccentricity: | 0.0021327 |
| inclination: | 49.9657° |
| perigee height: | 608 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 231.8419° |
| argument of perigee: | 254.4304° |
| revolutions per day: | 14.82076915 |
| mean anomaly at epoch: | 105.4279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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