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 16792U 26040.65269976 +.00000000 +00000-0 +56133-4 0 00002
2 16792 82.4813 106.6775 0022138 323.8311 36.1406 14.85563160 01
| Epoch (UTC): | 09 February 2026 15:39:53 |
| Eccentricity: | 0.0022138 |
| inclination: | 82.4813° |
| perigee height: | 596 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 106.6775° |
| argument of perigee: | 323.8311° |
| revolutions per day: | 14.85563160 |
| mean anomaly at epoch: | 36.1406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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