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 66018U 26145.18662434 +.00000000 +00000-0 +78463-3 0 00007
2 66018 53.1571 108.8654 0001086 86.2079 273.9046 15.30207907 09
| Epoch (UTC): | 25 May 2026 04:28:44 |
| Eccentricity: | 0.0001086 |
| inclination: | 53.1571° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.8654° |
| argument of perigee: | 86.2079° |
| revolutions per day: | 15.30207907 |
| mean anomaly at epoch: | 273.9046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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