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 63436U 26145.27156759 +.00000000 +00000-0 +58658-3 0 00000
2 63436 53.1584 144.3560 0001066 88.4979 271.6149 15.42172925 09
| Epoch (UTC): | 25 May 2026 06:31:03 |
| Eccentricity: | 0.0001066 |
| inclination: | 53.1584° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 144.3560° |
| argument of perigee: | 88.4979° |
| revolutions per day: | 15.42172925 |
| mean anomaly at epoch: | 271.6149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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