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 64008U 26145.65176076 +.00000000 +00000-0 +59077-3 0 00008
2 64008 42.9998 283.4895 0001079 247.2850 112.7888 15.27596384 00
| Epoch (UTC): | 25 May 2026 15:38:32 |
| Eccentricity: | 0.0001079 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 283.4895° |
| argument of perigee: | 247.2850° |
| revolutions per day: | 15.27596384 |
| mean anomaly at epoch: | 112.7888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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