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 26019.65980259 +.00000000 +00000-0 +12110-3 0 00006
2 10967 108.0164 22.6019 0001205 281.3579 78.7431 14.46106972 08
| Epoch (UTC): | 19 January 2026 15:50:06 |
| Eccentricity: | 0.0001205 |
| inclination: | 108.0164° |
| perigee height: | 738 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 22.6019° |
| argument of perigee: | 281.3579° |
| revolutions per day: | 14.46106972 |
| mean anomaly at epoch: | 78.7431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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