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 64109U 26145.41580360 +.00000000 +00000-0 +66770-3 0 00007
2 64109 53.1613 30.0891 0001268 83.0113 277.1032 15.31716655 07
| Epoch (UTC): | 25 May 2026 09:58:45 |
| Eccentricity: | 0.0001268 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 30.0891° |
| argument of perigee: | 83.0113° |
| revolutions per day: | 15.31716655 |
| mean anomaly at epoch: | 277.1032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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