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 66644U 26145.37840208 +.00000000 +00000-0 +22543-3 0 00008
2 66644 53.1597 144.0284 0001107 88.8364 271.2763 15.30199906 08
| Epoch (UTC): | 25 May 2026 09:04:53 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.0284° |
| argument of perigee: | 88.8364° |
| revolutions per day: | 15.30199906 |
| mean anomaly at epoch: | 271.2763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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