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 00116U 26045.78192825 +.00000000 +00000-0 +73120-4 0 00007
2 00116 66.8086 190.3474 0075960 353.8622 6.1519 13.92307358 01
| Epoch (UTC): | 14 February 2026 18:45:58 |
| Eccentricity: | 0.0075960 |
| inclination: | 66.8086° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 190.3474° |
| argument of perigee: | 353.8622° |
| revolutions per day: | 13.92307358 |
| mean anomaly at epoch: | 6.1519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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