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 26041.21560488 +.00000000 +00000-0 +65844-4 0 00008
2 11267 82.5252 122.6397 0016980 145.0466 215.1872 14.91874432 02
| Epoch (UTC): | 10 February 2026 05:10:28 |
| Eccentricity: | 0.0016980 |
| inclination: | 82.5252° |
| perigee height: | 580 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 122.6397° |
| argument of perigee: | 145.0466° |
| revolutions per day: | 14.91874432 |
| mean anomaly at epoch: | 215.1872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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