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 26044.72476806 +.00000000 +00000-0 +10599-3 0 00000
2 11327 82.9488 106.8472 0026547 325.4335 155.6135 13.77197212 08
| Epoch (UTC): | 13 February 2026 17:23:39 |
| Eccentricity: | 0.0026547 |
| inclination: | 82.9488° |
| perigee height: | 954 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 106.8472° |
| argument of perigee: | 325.4335° |
| revolutions per day: | 13.77197212 |
| mean anomaly at epoch: | 155.6135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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