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 64002U 26145.66461036 +.00000000 +00000-0 +67547-3 0 00007
2 64002 43.0024 283.5937 0001636 273.3359 86.7305 15.27599487 08
| Epoch (UTC): | 25 May 2026 15:57:02 |
| Eccentricity: | 0.0001636 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 283.5937° |
| argument of perigee: | 273.3359° |
| revolutions per day: | 15.27599487 |
| mean anomaly at epoch: | 86.7305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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