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 64260U 26144.94969931 +.00000000 +00000-0 +61828-3 0 00006
2 64260 53.1587 120.2199 0001460 226.6158 133.4723 15.35348972 04
| Epoch (UTC): | 24 May 2026 22:47:34 |
| Eccentricity: | 0.0001460 |
| inclination: | 53.1587° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 120.2199° |
| argument of perigee: | 226.6158° |
| revolutions per day: | 15.35348972 |
| mean anomaly at epoch: | 133.4723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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