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 11327U 26017.32121600 +.00000000 +00000-0 +25430-4 0 00006
2 11327 82.9519 127.1979 0028253 42.1568 11.5791 13.77191615 07
| Epoch (UTC): | 17 January 2026 07:42:33 |
| Eccentricity: | 0.0028253 |
| inclination: | 82.9519° |
| perigee height: | 953 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 127.1979° |
| argument of perigee: | 42.1568° |
| revolutions per day: | 13.77191615 |
| mean anomaly at epoch: | 11.5791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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