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 26156.46888240 +.00000000 +00000-0 +30271-3 0 00009
2 16986 82.5241 149.5521 0003497 240.4486 119.6409 15.35069996 05
| Epoch (UTC): | 05 June 2026 11:15:11 |
| Eccentricity: | 0.0003497 |
| inclination: | 82.5241° |
| perigee height: | 458 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 149.5521° |
| argument of perigee: | 240.4486° |
| revolutions per day: | 15.35069996 |
| mean anomaly at epoch: | 119.6409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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