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 66010U 26145.61140581 +.00000000 +00000-0 +49688-3 0 00008
2 66010 53.1610 106.5418 0001356 102.0596 258.0559 15.34399874 01
| Epoch (UTC): | 25 May 2026 14:40:25 |
| Eccentricity: | 0.0001356 |
| inclination: | 53.1610° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 106.5418° |
| argument of perigee: | 102.0596° |
| revolutions per day: | 15.34399874 |
| mean anomaly at epoch: | 258.0559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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