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 26039.67295712 +.00000000 +00000-0 +73602-4 0 00001
2 11267 82.5253 124.1030 0016824 149.9544 210.2645 14.91872200 06
| Epoch (UTC): | 08 February 2026 16:09:03 |
| Eccentricity: | 0.0016824 |
| inclination: | 82.5253° |
| perigee height: | 580 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 124.1030° |
| argument of perigee: | 149.9544° |
| revolutions per day: | 14.91872200 |
| mean anomaly at epoch: | 210.2645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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