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 26128.20411985 +.00000000 +00000-0 +41121-4 0 00002
2 11267 82.5262 40.0931 0015005 214.0842 145.9416 14.91979571 06
| Epoch (UTC): | 08 May 2026 04:53:55 |
| Eccentricity: | 0.0015005 |
| inclination: | 82.5262° |
| perigee height: | 581 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 40.0931° |
| argument of perigee: | 214.0842° |
| revolutions per day: | 14.91979571 |
| mean anomaly at epoch: | 145.9416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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