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 64526U 26145.43725590 +.00000000 +00000-0 +72169-4 0 00008
2 64526 51.8999 198.6163 0000247 6.4901 353.6064 14.79933728 03
| Epoch (UTC): | 25 May 2026 10:29:38 |
| Eccentricity: | 0.0000247 |
| inclination: | 51.8999° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 198.6163° |
| argument of perigee: | 6.4901° |
| revolutions per day: | 14.79933728 |
| mean anomaly at epoch: | 353.6064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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