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 66226U 26145.58335647 +.00000000 +00000-0 +10966-2 0 00008
2 66226 53.1602 232.6714 0001585 78.0460 270.3091 15.33557071 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001585 |
| inclination: | 53.1602° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 232.6714° |
| argument of perigee: | 78.0460° |
| revolutions per day: | 15.33557071 |
| mean anomaly at epoch: | 270.3091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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