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 26041.47193916 +.00000000 +00000-0 +85509-4 0 00005
2 00116 66.8081 200.8932 0075614 356.8824 3.1774 13.92306411 04
| Epoch (UTC): | 10 February 2026 11:19:35 |
| Eccentricity: | 0.0075614 |
| inclination: | 66.8081° |
| perigee height: | 865 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 200.8932° |
| argument of perigee: | 356.8824° |
| revolutions per day: | 13.92306411 |
| mean anomaly at epoch: | 3.1774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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