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 26044.70443125 +.00000000 +00000-0 +72510-4 0 00002
2 00116 66.8085 192.9838 0075874 354.6110 5.4144 13.92307079 03
| Epoch (UTC): | 13 February 2026 16:54:22 |
| Eccentricity: | 0.0075874 |
| inclination: | 66.8085° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 192.9838° |
| argument of perigee: | 354.6110° |
| revolutions per day: | 13.92307079 |
| mean anomaly at epoch: | 5.4144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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