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 26048.58341950 +.00000000 +00000-0 +69714-4 0 00007
2 00116 66.8090 183.4931 0076200 351.9078 8.0766 13.92308027 08
| Epoch (UTC): | 17 February 2026 14:00:07 |
| Eccentricity: | 0.0076200 |
| inclination: | 66.8090° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 183.4931° |
| argument of perigee: | 351.9078° |
| revolutions per day: | 13.92308027 |
| mean anomaly at epoch: | 8.0766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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