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 26088.14091925 +.00000000 +00000-0 +11804-3 0 00008
2 10967 108.0075 166.3129 0002662 276.1081 83.9761 14.46176067 01
| Epoch (UTC): | 29 March 2026 03:22:55 |
| Eccentricity: | 0.0002662 |
| inclination: | 108.0075° |
| perigee height: | 736 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 166.3129° |
| argument of perigee: | 276.1081° |
| revolutions per day: | 14.46176067 |
| mean anomaly at epoch: | 83.9761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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