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 18665U 26040.40813104 +.00000000 +00000-0 +60810-4 0 00001
2 18665 66.0845 23.5241 0036155 191.6809 168.3462 14.55611678 02
| Epoch (UTC): | 09 February 2026 09:47:42 |
| Eccentricity: | 0.0036155 |
| inclination: | 66.0845° |
| perigee height: | 682 km |
| apogee height: | 733 km |
| right ascension of ascending node: | 23.5241° |
| argument of perigee: | 191.6809° |
| revolutions per day: | 14.55611678 |
| mean anomaly at epoch: | 168.3462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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