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 64522U 26145.54947027 +.00000000 +00000-0 +50405-3 0 00005
2 64522 51.8957 250.7206 0000297 95.9066 264.1930 14.79939011 00
| Epoch (UTC): | 25 May 2026 13:11:14 |
| Eccentricity: | 0.0000297 |
| inclination: | 51.8957° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 250.7206° |
| argument of perigee: | 95.9066° |
| revolutions per day: | 14.79939011 |
| mean anomaly at epoch: | 264.1930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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