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 26128.17081816 +.00000000 +00000-0 +48163-3 0 00007
2 16326 82.4863 209.8569 0002601 121.7795 238.3723 15.74136103 00
| Epoch (UTC): | 08 May 2026 04:05:58 |
| Eccentricity: | 0.0002601 |
| inclination: | 82.4863° |
| perigee height: | 345 km |
| apogee height: | 349 km |
| right ascension of ascending node: | 209.8569° |
| argument of perigee: | 121.7795° |
| revolutions per day: | 15.74136103 |
| mean anomaly at epoch: | 238.3723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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