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 26047.14675740 +.00000000 +00000-0 +82794-4 0 00008
2 00116 66.8088 187.0081 0076070 352.9155 7.0842 13.92307822 09
| Epoch (UTC): | 16 February 2026 03:31:19 |
| Eccentricity: | 0.0076070 |
| inclination: | 66.8088° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 187.0081° |
| argument of perigee: | 352.9155° |
| revolutions per day: | 13.92307822 |
| mean anomaly at epoch: | 7.0842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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