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 64563U 26145.56586272 +.00000000 +00000-0 +47104-3 0 00005
2 64563 97.7647 260.6112 0002237 15.6472 344.4818 14.96840305 05
| Epoch (UTC): | 25 May 2026 13:34:50 |
| Eccentricity: | 0.0002237 |
| inclination: | 97.7647° |
| perigee height: | 575 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 260.6112° |
| argument of perigee: | 15.6472° |
| revolutions per day: | 14.96840305 |
| mean anomaly at epoch: | 344.4818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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