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 26049.73274897 +.00000000 +00000-0 +82128-4 0 00004
2 00116 66.8091 180.6810 0076287 351.1029 8.8692 13.92308320 09
| Epoch (UTC): | 18 February 2026 17:35:09 |
| Eccentricity: | 0.0076287 |
| inclination: | 66.8091° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 180.6810° |
| argument of perigee: | 351.1029° |
| revolutions per day: | 13.92308320 |
| mean anomaly at epoch: | 8.8692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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