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 64509U 26145.58592507 +.00000000 +00000-0 +10156-3 0 00002
2 64509 51.8973 247.9967 0000338 104.6596 255.4404 14.79931878 09
| Epoch (UTC): | 25 May 2026 14:03:43 |
| Eccentricity: | 0.0000338 |
| inclination: | 51.8973° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 247.9967° |
| argument of perigee: | 104.6596° |
| revolutions per day: | 14.79931878 |
| mean anomaly at epoch: | 255.4404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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