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 11267U 26130.48439198 +.00000000 +00000-0 +28067-4 0 00005
2 11267 82.5264 37.9300 0015192 206.0893 153.9563 14.91981108 08
| Epoch (UTC): | 10 May 2026 11:37:31 |
| Eccentricity: | 0.0015192 |
| inclination: | 82.5264° |
| perigee height: | 581 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 37.9300° |
| argument of perigee: | 206.0893° |
| revolutions per day: | 14.91981108 |
| mean anomaly at epoch: | 153.9563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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