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 64487U 26145.22406971 +.00000000 +00000-0 +19329-2 0 00007
2 64487 53.1553 121.4748 0001483 31.0390 329.0698 15.30210916 07
| Epoch (UTC): | 25 May 2026 05:22:39 |
| Eccentricity: | 0.0001483 |
| inclination: | 53.1553° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 121.4748° |
| argument of perigee: | 31.0390° |
| revolutions per day: | 15.30210916 |
| mean anomaly at epoch: | 329.0698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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