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 64263U 26145.34091578 +.00000000 +00000-0 +87981-3 0 00005
2 64263 53.1574 120.5245 0001149 77.5112 282.6018 15.30203327 08
| Epoch (UTC): | 25 May 2026 08:10:55 |
| Eccentricity: | 0.0001149 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.5245° |
| argument of perigee: | 77.5112° |
| revolutions per day: | 15.30203327 |
| mean anomaly at epoch: | 282.6018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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