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 66640U 26145.25610286 +.00000000 +00000-0 +49394-3 0 00005
2 66640 53.1607 143.9794 0001053 75.9009 284.2109 15.30210606 02
| Epoch (UTC): | 25 May 2026 06:08:47 |
| Eccentricity: | 0.0001053 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.9794° |
| argument of perigee: | 75.9009° |
| revolutions per day: | 15.30210606 |
| mean anomaly at epoch: | 284.2109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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