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 64009U 26145.35937825 +.00000000 +00000-0 +13783-2 0 00006
2 64009 42.9991 284.7291 0001499 160.8268 199.2640 15.27631697 00
| Epoch (UTC): | 25 May 2026 08:37:30 |
| Eccentricity: | 0.0001499 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 284.7291° |
| argument of perigee: | 160.8268° |
| revolutions per day: | 15.27631697 |
| mean anomaly at epoch: | 199.2640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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