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 64387U 26144.35845880 +.00000000 +00000-0 +24059-3 0 00002
2 64387 43.0028 112.0947 0001133 283.8149 76.2576 15.27581289 05
| Epoch (UTC): | 24 May 2026 08:36:10 |
| Eccentricity: | 0.0001133 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 112.0947° |
| argument of perigee: | 283.8149° |
| revolutions per day: | 15.27581289 |
| mean anomaly at epoch: | 76.2576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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