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 26037.68903284 +.00000000 +00000-0 +68769-4 0 00006
2 16792 82.4818 109.4773 0022374 333.9709 26.0380 14.85560379 08
| Epoch (UTC): | 06 February 2026 16:32:12 |
| Eccentricity: | 0.0022374 |
| inclination: | 82.4818° |
| perigee height: | 596 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 109.4773° |
| argument of perigee: | 333.9709° |
| revolutions per day: | 14.85560379 |
| mean anomaly at epoch: | 26.0380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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