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 66627U 26145.22668512 +.00000000 +00000-0 +23998-3 0 00004
2 66627 53.1574 144.5121 0001271 89.3260 270.7886 15.30179009 04
| Epoch (UTC): | 25 May 2026 05:26:25 |
| Eccentricity: | 0.0001271 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.5121° |
| argument of perigee: | 89.3260° |
| revolutions per day: | 15.30179009 |
| mean anomaly at epoch: | 270.7886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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