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 14680U 26161.32462708 +.00000000 +00000-0 +98977-5 0 00005
2 14680 82.9561 129.6834 0036423 236.9545 233.6346 13.76725744 00
| Epoch (UTC): | 10 June 2026 07:47:27 |
| Eccentricity: | 0.0036423 |
| inclination: | 82.9561° |
| perigee height: | 949 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 129.6834° |
| argument of perigee: | 236.9545° |
| revolutions per day: | 13.76725744 |
| mean anomaly at epoch: | 233.6346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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