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 63734U 26145.32805432 +.00000000 +00000-0 +29092-3 0 00006
2 63734 51.8985 120.4620 0000529 161.3247 198.7735 14.79928633 08
| Epoch (UTC): | 25 May 2026 07:52:23 |
| Eccentricity: | 0.0000529 |
| inclination: | 51.8985° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 120.4620° |
| argument of perigee: | 161.3247° |
| revolutions per day: | 14.79928633 |
| mean anomaly at epoch: | 198.7735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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