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 64500U 26145.00653775 +.00000000 +00000-0 +22706-3 0 00009
2 64500 51.9001 255.6295 0000357 113.8412 246.2588 14.79936619 02
| Epoch (UTC): | 25 May 2026 00:09:24 |
| Eccentricity: | 0.0000357 |
| inclination: | 51.9001° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 255.6295° |
| argument of perigee: | 113.8412° |
| revolutions per day: | 14.79936619 |
| mean anomaly at epoch: | 246.2588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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