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 63731U 26145.28255810 +.00000000 +00000-0 +18781-3 0 00000
2 63731 51.8983 139.4303 0000567 41.6072 318.4934 14.79942147 07
| Epoch (UTC): | 25 May 2026 06:46:53 |
| Eccentricity: | 0.0000567 |
| inclination: | 51.8983° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 139.4303° |
| argument of perigee: | 41.6072° |
| revolutions per day: | 14.79942147 |
| mean anomaly at epoch: | 318.4934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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