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 64105U 26145.10856072 +.00000000 +00000-0 +29197-3 0 00007
2 64105 53.1591 31.7287 0001104 86.3103 273.8025 15.31694682 09
| Epoch (UTC): | 25 May 2026 02:36:19 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 31.7287° |
| argument of perigee: | 86.3103° |
| revolutions per day: | 15.31694682 |
| mean anomaly at epoch: | 273.8025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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