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 26040.09287889 +.00000000 +00000-0 +29180-3 0 00009
2 16986 82.5243 267.3088 0005197 323.4526 36.6361 15.32653664 03
| Epoch (UTC): | 09 February 2026 02:13:44 |
| Eccentricity: | 0.0005197 |
| inclination: | 82.5243° |
| perigee height: | 464 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 267.3088° |
| argument of perigee: | 323.4526° |
| revolutions per day: | 15.32653664 |
| mean anomaly at epoch: | 36.6361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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