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 64231U 26145.57879214 +.00000000 +00000-0 +31493-3 0 00003
2 64231 58.9930 223.7962 0010313 25.2455 334.9123 15.38030094 02
| Epoch (UTC): | 25 May 2026 13:53:27 |
| Eccentricity: | 0.0010313 |
| inclination: | 58.9930° |
| perigee height: | 445 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 223.7962° |
| argument of perigee: | 25.2455° |
| revolutions per day: | 15.38030094 |
| mean anomaly at epoch: | 334.9123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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