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 26162.36026593 +.00000000 +00000-0 +99203-4 0 00004
2 10967 108.0166 322.0574 0001981 240.6897 119.4051 14.46238845 01
| Epoch (UTC): | 11 June 2026 08:38:46 |
| Eccentricity: | 0.0001981 |
| inclination: | 108.0166° |
| perigee height: | 737 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 322.0574° |
| argument of perigee: | 240.6897° |
| revolutions per day: | 14.46238845 |
| mean anomaly at epoch: | 119.4051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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