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 66110U 26145.19926994 +.00000000 +00000-0 +63803-3 0 00007
2 66110 53.1571 108.8397 0001259 90.2641 269.8504 15.30207680 09
| Epoch (UTC): | 25 May 2026 04:46:56 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.1571° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.8397° |
| argument of perigee: | 90.2641° |
| revolutions per day: | 15.30207680 |
| mean anomaly at epoch: | 269.8504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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