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 66328U 26145.46862005 +.00000000 +00000-0 +65523-3 0 00001
2 66328 42.9999 139.1756 0001362 271.5918 88.4778 15.27591891 06
| Epoch (UTC): | 25 May 2026 11:14:48 |
| Eccentricity: | 0.0001362 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.1756° |
| argument of perigee: | 271.5918° |
| revolutions per day: | 15.27591891 |
| mean anomaly at epoch: | 88.4778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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