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 26042.22167806 +.00000000 +00000-0 +63677-4 0 00009
2 11267 82.5250 121.6854 0017056 141.8979 218.3451 14.91875980 02
| Epoch (UTC): | 11 February 2026 05:19:12 |
| Eccentricity: | 0.0017056 |
| inclination: | 82.5250° |
| perigee height: | 580 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 121.6854° |
| argument of perigee: | 141.8979° |
| revolutions per day: | 14.91875980 |
| mean anomaly at epoch: | 218.3451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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