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 26042.05150466 +.00000000 +00000-0 +29630-3 0 00007
2 16986 82.5243 265.3302 0005036 315.0374 45.0460 15.32692050 06
| Epoch (UTC): | 11 February 2026 01:14:10 |
| Eccentricity: | 0.0005036 |
| inclination: | 82.5243° |
| perigee height: | 464 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 265.3302° |
| argument of perigee: | 315.0374° |
| revolutions per day: | 15.32692050 |
| mean anomaly at epoch: | 45.0460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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