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 26159.46736347 +.00000000 +00000-0 +24776-3 0 00005
2 16986 82.5244 146.5127 0003741 225.1307 134.9632 15.35130113 09
| Epoch (UTC): | 08 June 2026 11:13:00 |
| Eccentricity: | 0.0003741 |
| inclination: | 82.5244° |
| perigee height: | 458 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 146.5127° |
| argument of perigee: | 225.1307° |
| revolutions per day: | 15.35130113 |
| mean anomaly at epoch: | 134.9632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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