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 64484U 26145.62437762 +.00000000 +00000-0 +56669-3 0 00009
2 64484 53.1570 119.7114 0001497 74.6354 285.4813 15.30210313 03
| Epoch (UTC): | 25 May 2026 14:59:06 |
| Eccentricity: | 0.0001497 |
| inclination: | 53.1570° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 119.7114° |
| argument of perigee: | 74.6354° |
| revolutions per day: | 15.30210313 |
| mean anomaly at epoch: | 285.4813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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