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 10967U 26150.39408233 +.00000000 +00000-0 +15523-3 0 00001
2 10967 108.0149 296.9407 0002290 243.9259 116.1652 14.46227883 09
| Epoch (UTC): | 30 May 2026 09:27:28 |
| Eccentricity: | 0.0002290 |
| inclination: | 108.0149° |
| perigee height: | 736 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 296.9407° |
| argument of perigee: | 243.9259° |
| revolutions per day: | 14.46227883 |
| mean anomaly at epoch: | 116.1652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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