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 64386U 26144.94822189 +.00000000 +00000-0 +47439-3 0 00000
2 64386 42.9998 108.7808 0000720 254.1133 105.9639 15.27589461 01
| Epoch (UTC): | 24 May 2026 22:45:26 |
| Eccentricity: | 0.0000720 |
| inclination: | 42.9998° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 108.7808° |
| argument of perigee: | 254.1133° |
| revolutions per day: | 15.27589461 |
| mean anomaly at epoch: | 105.9639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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