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 66622U 26145.29830462 +.00000000 +00000-0 +37367-3 0 00006
2 66622 53.1567 144.2438 0000375 29.9735 330.1287 15.30212900 04
| Epoch (UTC): | 25 May 2026 07:09:33 |
| Eccentricity: | 0.0000375 |
| inclination: | 53.1567° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 144.2438° |
| argument of perigee: | 29.9735° |
| revolutions per day: | 15.30212900 |
| mean anomaly at epoch: | 330.1287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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