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 64488U 26145.35150734 +.00000000 +00000-0 +59655-3 0 00002
2 64488 53.1576 120.8538 0001242 92.8245 267.2898 15.30211723 02
| Epoch (UTC): | 25 May 2026 08:26:10 |
| Eccentricity: | 0.0001242 |
| inclination: | 53.1576° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.8538° |
| argument of perigee: | 92.8245° |
| revolutions per day: | 15.30211723 |
| mean anomaly at epoch: | 267.2898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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