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 26100.17669583 +.00000000 +00000-0 +12147-3 0 00008
2 10967 108.0068 191.5640 0002787 269.7474 90.3353 14.46189357 08
| Epoch (UTC): | 10 April 2026 04:14:26 |
| Eccentricity: | 0.0002787 |
| inclination: | 108.0068° |
| perigee height: | 736 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 191.5640° |
| argument of perigee: | 269.7474° |
| revolutions per day: | 14.46189357 |
| mean anomaly at epoch: | 90.3353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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