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 66081U 26145.32540997 +.00000000 +00000-0 +84824-3 0 00000
2 66081 53.1556 248.6699 0001093 73.0838 287.0284 15.31717035 08
| Epoch (UTC): | 25 May 2026 07:48:35 |
| Eccentricity: | 0.0001093 |
| inclination: | 53.1556° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 248.6699° |
| argument of perigee: | 73.0838° |
| revolutions per day: | 15.31717035 |
| mean anomaly at epoch: | 287.0284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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