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 26037.67717222 +.00000000 +00000-0 +35612-3 0 00005
2 16986 82.5240 269.7494 0005488 333.7365 26.3598 15.32607499 08
| Epoch (UTC): | 06 February 2026 16:15:07 |
| Eccentricity: | 0.0005488 |
| inclination: | 82.5240° |
| perigee height: | 464 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 269.7494° |
| argument of perigee: | 333.7365° |
| revolutions per day: | 15.32607499 |
| mean anomaly at epoch: | 26.3598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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