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 26110.50326064 +.00000000 +00000-0 +77175-4 0 00008
2 00116 66.8114 31.9807 0080684 310.2375 49.1665 13.92322045 03
| Epoch (UTC): | 20 April 2026 12:04:41 |
| Eccentricity: | 0.0080684 |
| inclination: | 66.8114° |
| perigee height: | 862 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 31.9807° |
| argument of perigee: | 310.2375° |
| revolutions per day: | 13.92322045 |
| mean anomaly at epoch: | 49.1665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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