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 26042.13453126 +.00000000 +00000-0 +51659-4 0 00007
2 16792 82.4810 105.2776 0022035 318.7035 41.2514 14.85564559 06
| Epoch (UTC): | 11 February 2026 03:13:43 |
| Eccentricity: | 0.0022035 |
| inclination: | 82.4810° |
| perigee height: | 596 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 105.2776° |
| argument of perigee: | 318.7035° |
| revolutions per day: | 14.85564559 |
| mean anomaly at epoch: | 41.2514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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