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 16326U 26040.77835219 +.00000000 +00000-0 +54593-3 0 00004
2 16326 82.4909 303.5059 0006114 61.5294 298.6580 15.63798673 09
| Epoch (UTC): | 09 February 2026 18:40:49 |
| Eccentricity: | 0.0006114 |
| inclination: | 82.4909° |
| perigee height: | 373 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 303.5059° |
| argument of perigee: | 61.5294° |
| revolutions per day: | 15.63798673 |
| mean anomaly at epoch: | 298.6580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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