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 26064.89915727 +.00000000 +00000-0 +10448-3 0 00002
2 10967 108.0117 117.5457 0002237 286.7663 73.3237 14.46156247 00
| Epoch (UTC): | 05 March 2026 21:34:47 |
| Eccentricity: | 0.0002237 |
| inclination: | 108.0117° |
| perigee height: | 737 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 117.5457° |
| argument of perigee: | 286.7663° |
| revolutions per day: | 14.46156247 |
| mean anomaly at epoch: | 73.3237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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