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 16986U 26041.65978308 +.00000000 +00000-0 +28589-3 0 00007
2 16986 82.5243 265.7259 0005063 316.6833 43.4010 15.32684507 09
| Epoch (UTC): | 10 February 2026 15:50:05 |
| Eccentricity: | 0.0005063 |
| inclination: | 82.5243° |
| perigee height: | 464 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 265.7259° |
| argument of perigee: | 316.6833° |
| revolutions per day: | 15.32684507 |
| mean anomaly at epoch: | 43.4010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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