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 26065.31419147 +.00000000 +00000-0 +12374-3 0 00005
2 10967 108.0117 118.4166 0002255 286.3737 73.7161 14.46156977 05
| Epoch (UTC): | 06 March 2026 07:32:26 |
| Eccentricity: | 0.0002255 |
| inclination: | 108.0117° |
| perigee height: | 737 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 118.4166° |
| argument of perigee: | 286.3737° |
| revolutions per day: | 14.46156977 |
| mean anomaly at epoch: | 73.7161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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