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 66615U 26145.56112941 +.00000000 +00000-0 +50896-3 0 00005
2 66615 43.0002 341.9418 0000735 255.3515 104.7255 15.27599067 01
| Epoch (UTC): | 25 May 2026 13:28:01 |
| Eccentricity: | 0.0000735 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 341.9418° |
| argument of perigee: | 255.3515° |
| revolutions per day: | 15.27599067 |
| mean anomaly at epoch: | 104.7255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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